Multi wavelength electromagnetic device

ABSTRACT

An optical antenna assembly including multiple optical antenna elements, each of the optical antenna elements are arranged in a regular pattern and carried by a supporting body. The regular pattern of the plurality of optical antenna elements is nonuniform. Certain ones of the optical antenna elements are configured to respond to the one or more waves of light.

CROSS-REFERENCE TO RELATED APPLICATIONS

The present application is related to, claims the earliest availableeffective filing date(s) from (e.g., claims earliest available prioritydates for other than provisional patent applications; claims benefitsunder 35 USC § 119(e) for provisional patent applications), andincorporates by reference in its entirety all subject matter of thefollowing listed application(s) (the “Related Applications”) to theextent such subject matter is not inconsistent herewith; the presentapplication also claims the earliest available effective filing date(s)from, and also incorporates by reference in its entirety all subjectmatter of any and all parent, grandparent, great-grandparent, etc.applications of the Related Application(s) to the extent such subjectmatter is not inconsistent herewith. The United States Patent Office(USPTO) has published a notice to the effect that the USPTO's computerprograms require that patent applicants reference both a serial numberand indicate whether an application is a continuation or continuation inpart. The present applicant entity has provided below a specificreference to the application(s) from which priority is being claimed asrecited by statute. Applicant entity understands that the statute isunambiguous in its specific reference language and does not requireeither a serial number or any characterization such as “continuation” or“continuation-in-part.” Notwithstanding the foregoing, applicant entityunderstands that the USPTO's computer programs have certain data entryrequirements, and hence applicant entity is designating the presentapplication as a continuation in part of its parent applications, butexpressly points out that such designations are not to be construed inany way as any type of commentary and/or admission as to whether or notthe present application contains any new matter in addition to thematter of its parent application(s).

RELATED APPLICATIONS

1. For purposes of the USPTO extra-statutory requirements, the presentapplication constitutes a continuation-in-part of United States patentapplication Ser. No. 11/069,593, entitled OPTICAL ANTENNA ASSEMBLY,naming W. Daniel Hillis, Nathan P. Myhrvold, Clarence T. Tegreene andLowell L. Wood, Jr., as inventors, filed Feb. 28, 2005.

2. For purposes of the USPTO extra-statutory requirements, the presentapplication constitutes a continuation-in-part of United States patentapplication Ser. No. 11/263,539, entitled ELECTROMAGNETIC DEVICE WITHINTEGRAL NON-LINEAR COMPONENT, naming W. Daniel Hillis, Nathan P.Myhrvold, Clarence T. Tegreene and Lowell L. Wood, Jr., as inventors,filed Oct. 31, 2005.

3. For purposes of the USPTO extra-statutory requirements, the presentapplication constitutes a continuation-in-part of United States patentapplication Ser. No. 11/263,554, entitled OPTICAL ANTENNA WITH PHASECONTROL, naming W. Daniel Hillis, Nathan P. Myhrvold, Clarence T.Tegreene and Lowell L. Wood, Jr., as inventors, filed Oct. 31, 2005.

4. For purposes of the USPTO extra-statutory requirements, the presentapplication constitutes a continuation-in-part of United States patentapplication Ser. No. 11/263,540, entitled ELECTROMAGNETIC DEVICE WITHFREQUENCY DOWNCONVERTER, naming W. Daniel Hillis, Nathan P. Myhrvold,Clarence T. Tegreene and Lowell L. Wood, Jr., as inventors, filed Oct.31, 2005.

5. For purposes of the USPTO extra-statutory requirements, the presentapplication constitutes a continuation-in-part of United States patentapplication Ser. No. 11/263,656, entitled OPTICAL ANTENNA WITH OPTICALREFERENCE, naming W. Daniel Hillis, Nathan P. Myhrvold, Clarence T.Tegreene and Lowell L. Wood, Jr., as inventors, filed Oct. 31, 2005.

TECHNICAL FIELD

The present application relates, in general, to antennas and relatedcomponents and systems, at or near, optical frequencies.

BRIEF DESCRIPTION OF THE FIGURES

FIG. 1 is a schematic diagram of one embodiment of an optical antennaassembly that is configured to receive optical energy;

FIG. 2 is a schematic diagram of another embodiment of an opticalantenna assembly that is configured to emit light;

FIG. 3 is a generalized cross sectional diagram of a portion of oneembodiment of an optical antenna assembly;

FIG. 4 is a perspective view of a portion of another embodiment of anoptical antenna assembly;

FIG. 5 a is an isometric representation of a portion of anotherembodiment of an optical antenna assembly that is produced withnanotubes;

FIG. 5 b is a top view of one of the optical antenna elements of theoptical antenna assembly that is shown in FIG. 5 a;

FIG. 6 is a view of one embodiment of an interference pattern created bya plurality of optical antenna elements;

FIG. 7 is a view of another embodiment of an interference patterncreated by the plurality of optical antenna elements of FIG. 6, in whichthat relative phase of one of the optical antenna elements is shifted;

FIG. 8 is a side view of one embodiment of the optical antenna elementand an associated detector, in which the detector is configured as adiode;

FIG. 9 is a side view of another embodiment of the optical antennaelement and an associated detector, in which the detector is configuredas a transistor;

FIG. 10 is a side view of yet another embodiment of the optical antennaelement and an associated detector, in which the detector is configuredas a Schottky diode;

FIG. 11 is a general schematic view of one embodiment of an oscillatorcircuit that can be used to produce a signal;

FIG. 12 is a schematic diagram of feedback element;

FIG. 13 is a diagrammatic representation of a portion of an opticalantenna assembly having separate optical antenna elements positioned toreceive a reference signal;

FIG. 14 is a schematic diagram of one embodiment of an array ofreceiving optical antenna elements;

FIG. 15 is a schematic diagram of one embodiment of an array ofgenerating optical antenna elements;

FIG. 16 is a schematic diagram of another embodiment of optical antennaelements, including a reference planar waveform generator;

FIG. 17 is a top view of one embodiment of an optical antenna assembly;

FIG. 17 is a top view of another embodiment of an optical antennaassembly;

FIG. 18 is a top view of yet another embodiment of an optical antennaassembly;

FIG. 20 is a schematic diagram of one embodiment of an optical antennacontroller;

FIG. 21 is a view of one embodiment of an illumination system;

FIG. 22 is a diagrammatic representation of one embodiment of opticalantenna element arrangements; and

FIG. 23 is a schematic diagram of one embodiment of an arrangement ofoptical antenna elements according to grid.

DETAILED DESCRIPTION

This disclosure describes a number of embodiments of one or more opticalantenna elements that can be arranged in an optical antenna assembly.The optical antenna assembly may include an array of the optical antennaelements. Such arrays of optical antenna elements may, in certainembodiments, be spatially arranged in either a non-uniform or uniformpattern to provide the desired optical antenna assembly characteristicsand/or generate or receive light having a desired response. Theconfiguration of the arrays of optical antenna elements within theoptical antenna assembly may affect the shape, strength, operation, andcharacteristics of the waveform received by, or generated by, theoptical antenna assembly.

Optical antenna elements may be configured to either generate or receivelight. In actuality, the physical structure of a generating opticalantenna element can be identical to that of a receiving optical antennaelement. As such, a single optical antenna element, or an array of suchelements, can be used to generate and/or receive light. This disclosurethereby includes a description of the structure or the associatedcharacteristics of a number of embodiments of generating and receivingoptical antenna assemblies. The receiving optical antenna assembly, asdescribed with respect to FIG. 1, acts to convert received light (of thevisible or near-visible spectrum) into an electrical signal. Thegenerating optical antenna element, as described with respect to FIG. 2,converts an electrical signal into corresponding generated light.

Within this disclosure, the term “optical” as applied to the phrase“optical antenna” indicates that the antenna generates or receivesenergy, or otherwise interacts with energy, at or near opticalfrequencies. This light and/or energy can be converted to/fromelectrical signals that can be transported along conductive or similarpathways. The fundamental physics of such optical antenna elements cantherefore rely upon the conversion of energy between electromagneticwaves that travel through a medium such as air or a vacuum, andelectrical signals that travel along an electrically conductive orsimilar pathway, and/or vice versa. A number of publications that relateto nanostructures are described in the publication: “NANO-OPTICSPublications 1997-2005”; printed on Dec. 22, 2004; pp. 1-7; NanoopticsPublications; located at:http://nanooptics.uni-graz.at/ol/ol_publi.html.

Applications for optical antenna assemblies include, but are not limitedto, cameras, telescopes, beamformers, solar cells, detectors,projectors, and light sources.

In this disclosure, the terms “visible” or “optical” light, or simply“light” also relate in this disclosure to so-called “near-visible” lightsuch as that in the near infrared, infra-red, far infrared and the nearand far ultra-violet spectrums. Moreover, many principles herein may beextended to many spectra of electromagnetic radiation where theprocessing, electronic components, or other factors do not precludeoperation at such frequencies, including frequencies that may be outsideranges typically considered to be optical frequencies.

Within this disclosure, the term “regular”, when referring to aplurality or array of optical antenna elements, is not limited tosubstantially evenly spacing between or among various components.Moreover, regular spacing may be satisfied at the points of attachment,or other locations of components, that may not extend in parallel.Further, the dimensions of individual components may be small in manyembodiments, and minor deviations from exact placement or separation maystill be considered regular. Further, regular may pertain to spacings,features, separations, or other aspects of individual or groups ofcomponents.

Similarly, the term “uniform”, does not require exact uniformity ofsize, features, spacing, distribution or other aspects that may beconsidered to be uniform. Altering a configuration of optical antennaelements by reducing the probability of optical antenna elements formingthereat, forming shorter optical antenna elements in a particularregion, removing optical antenna elements from a particular region, etc.can have the effect of altering the optical characteristics of the ofthe optical antenna assembly.

To efficiently generate or receive light, the effective lengths of theoptical antenna elements usually equal some integer multiple of quarterwavelengths of the generated or received light (λ/4). The physicallength dimension of single wavelength versions of the optical antennaelements can approximately equal the effective wavelength of thegenerated or received light. Due to the minute wavelength of many of therelevant ranges of light, many embodiments of the optical antennaelements can be fabricated to be minute (e.g. such as within the micro-or nano-scale), and still allowing the antenna elements to couple withthe electromagnetic radiation that occurs at similar light wavelengthssuch as within the visible spectrum.

In some cases, optical antenna assemblies (including both those that areconfigured to receive light and/or generate light) can be designed toprovide a variety of efficiencies based largely on coherency of lightproduced by multiple included optical antenna elements and theircoherencies. Light from multiple coherently generating or receivingoptical antenna elements may be in phase at a number of locations or atvarious angular ranges. In such configurations, their wave amplitude mayadd or interfere coherently at one or more locations or angles relativeto the array of optical antenna element. In other applications, it maybe desirable to configure an optical antenna assembly to generate lightthat is out of phase at one or more spatial locations or angular rangesrelative to the optical antenna assembly, and therefore generate orreceive substantially incoherent light or partially coherent light atsome or all spatial locations or angular ranges relative to the array.

The relationship between two adjacent optical antenna elements such asexists in an antenna array is described herein to indicate how the lightfrom arrays of optical antenna elements constructively or destructivelyinterfere. This constructive and destructive interference is oftenrelevant to such optical antenna assembly issues as wave phases,beamforming, and beamsteering as described in this disclosure. Therelationship between the two adjacent optical antenna elements can beextended in principle to either uniform or non-uniform arrays dependingupon the desired waveform. Moreover, while such principles can berelevant to the operation, understanding, and/or characteristics of manyembodiments, a variety of other design principles may be employed insuch designs or analyses.

Light that is generated or received from pairs of proximally-locatedgenerating optical antenna elements or proximally-located receivingoptical antenna elements can destructively interfere at a number oflocations relative to the optical antenna elements, and light canconstructively interfere at other spatial locations. As such, therespective generating or receiving optical antenna elements can generateor receive light from one or more spatial locations or angular ranges.The relative phase relationships of the light that is generated orreceived by the optical antenna element largely dictates those spatiallocations, relative to the array, where the combined optical signal ismostly in phase and therefore the amplitude of the combined signals fromthe array of optical antenna elements contribute to be of the greatestintensity at each point along that region of the waveform. Destructiveinterference between proximate pairs of optical antenna elements canproduce a reduced amplitude or gain in corresponding regions.

Adjusting the relative phases of the generating or receiving opticalantenna elements can control gain along respective paths relative to theoptical antenna assembly at which the light is generated or received. Insome applications the phases may be controlled to produce a relativelyhigh gain along a limited range of directions. In an emissive case, thisprocess may be referred to as “beamforming”. An associated processinvolves changing the direction of gain. This process may be referred toas “beam steering”. Many embodiments of the optical antenna assembly canbe phased array optical devices that utilize beamforming and/orbeamsteering techniques.

In many embodiments, an optical antenna assembly 100 as described withrespect to both FIGS. 1 and 2, includes a number of the optical antennaelements 102 that can be arranged in a substantially planar array toform the optical antenna assembly 100, though the structures methods andsystems described herein are not limited to embodiments having planar orsubstantially planar arrangements. The arrangement of optical antennaelements 102 can be either regular or non-regular and can betwo-dimensional, or three-dimensional. In one approach, a threedimensional arrangement may be achieved by stacking two or moretwo-dimensional arrays. The arrangements of antenna elements and theconfiguration of individual optical antenna elements may be variedaccording to the principles described herein to produce a variety offrequency responses, beam patterns, or other operational properties.

Examples of Receiving Optical Antenna Assemblies

This portion of the disclosure describes a number of embodiments of areceiving optical antenna assembly as described with respect to FIG. 1.A subsequent portion of the disclosure describes a number of embodimentsof a generating optical antenna assembly, as described with respect toFIG. 2. Several embodiments of optical antenna assemblies, includingembodiments according to FIGS. 1 and 2, can be arranged in either areceiving or generating configuration, as described with respect toFIGS. 1, 2, 3, 4, 5 a, or 5 b. The relevance of having the arrays ofoptical antenna elements uniformly or non-uniformly spaced within theoptical antenna assemblies is described in this disclosure. Certainembodiments of the detector and light source configurations, by whichlight transitions to, or is transitioned from, electrical signals arealso described herein.

The optical antenna assembly 100 that is configured as a receiver can beapplied to a number of different applications including, but not limitedto, a light detector, a light sensor, a camera, etc. The optical antennaassembly 100 that is configured as a receiver includes a plurality ofoptical antenna elements 102 that can be each individually coupled to arespective phase adjust (“φ-adjust”) 104 via a respective guidingstructure, represented as an individual electrical conductor 105.Electrical signals can transit along the guiding structure from theφ-adjust 104 to a combiner 106.

One skilled in the art will recognize that a variety of approaches toguiding structures may be appropriate to carry signals to or from theantenna elements 102. One example of a nanoparticle waveguide isdescribed in the article J. R. Krenn; “Nanoparticle Waveguides WatchingEnergy Transfer”; News & Views; April 2003; pp. 1-2; Volume 2; NatureMaterials, incorporated herein by reference. An example of a techniqueto “squeeze” millimeter waves into a micron waveguide is described inthe article: A. P. Hibbins, J. R. Sambles; “Squeezing Millimeter Wavesinto Microns”; Physical Review Letters; Apr. 9, 2004; pp.143904-1/143904-4; Volume 92, Number 14; The American Physical Society,incorporated herein by reference. Additional references described andincorporated hereinbelow analyze and characterize the propagation ofenergy along various guiding structures, such as conductors, at higherfrequencies, including those at or near optical frequencies and thoserelating to propagation of plasmons along guiding structures. Some suchpathways may include conductors, may be formed from semiconductive ordielectric materials, or may include a combination thereof. Moreover,materials that may be characterized as dielectrics or conductors at onefrequency may operate very differently at other frequencies. The actualmaterial that carries or guides electrical signals or waves will dependupon a variety of factors, including the frequency of the energypropagating. Nevertheless, for clarity of the presentation for thecurrent portion of this description, the various guiding structures arerepresented diagrammatically and referred to herein as the electricalconductor 105, though the term conductor should not be considered to belimited to materials typically considered to be electrical conductors atrelatively low frequencies.

The φ-adjust 104 for each light-receiving optical antenna element 102 iscapable of adjusting the relative phase of the electrical signalrelative to light that is received as a signal formed by each particularoptical antenna element 102 at the combiner 106. The φ-adjusts 104 arepresented diagrammatically in FIGS. 1 and 2 for clarity of presentation.One skilled in the art will recognize that a variety of structures maybe implement the φ-adjust 104 functionality, including, in a relativelystraightforward implementation, waveguides having materials with fixedor electrically controllable effective dielectric constants and/oroptical transmission distances. Other various exemplary embodiments ofthe φ-adjust 104 will be described in more detail hereinbelow.

In one approach, the φ-adjust 104 controls the effective time requiredfor a signal to travel from the particular optical antenna element 102to the combiner 106, and therefore the relative phase of a signalcarried by the electrical conductor 105. By adjusting the relative phaseof signal traveling through each of the multiple φ-adjusts 104, therelative phases of the signals that can be applied from the opticalantenna elements 102 to the combiner can be adjusted.

In one embodiment, signals output from each φ-adjust 104 arrive at thecombiner 106 for each receiving optical antenna assembly 100. Oneφ-adjust 104 is associated with each light-receiving optical antennaelement 102, and the φ-adjust 104 is configured to adjust the relativephase of light being produced or received by functioning as a fixed orvariable delay element. It is thereby envisioned that in one embodiment,each φ-adjust 104 can be configured as a signal-delay component thatdelays the duration required for a signal to pass through the φ-adjust104 by some percentage of a wavelength of the light that is to bereceived or generated by other corresponding optical antenna elements102, thereby alternating the relative phases of the signals produced bythe different optical antenna elements.

The embodiments of the receiving optical antenna assembly 100 asdescribed with respect to FIG. 1 include the combiner 106 that mixes orotherwise combines signals from the different optical antenna elementsto provide an output signal (not shown) corresponding to the amount oflight energy received at the respective optical wavelength of eachoptical antenna element 102.

While the combiner 106 is presented diagrammatically as an operationalblock coupled to the φ-adjusts 104, one skilled in the art willrecognize that a variety of configurations may achieve the functionalityrealized by the combiner. Some such configurations may even employfree-space optical or RF (radio frequency) techniques to produce asignal that is a function of the signals from the φ-adjusts 104. In someconfigurations, the signal may be a combination of the signals from theφ-adjusts 104 or may be a nonlinear, square law or other function ofsuch signals, such as a down converted, square law combination, phase orfrequency modulated version, or even an integrated sum of such signals.

In some embodiments, the combiner 106 can be configured to include anadder circuit, a multiplier circuit, a mixer circuit, or some otherarithmetic configuration depending upon the functionality of the opticalantenna assembly 100. The combiner can also include a signal amplifierthat amplifies the signal strength that is applied to the combiner 106to a level (e.g., for certain prescribed frequencies) that is sufficientto transmit the signal to another device, or to an image processor thatmay identify information represented by the various signals. In manyembodiments, the combiner 106 can be associated with, or integratedinto, a computer device such as a signal processing portion of an analogor digital computer. As such, the computer device functions as a signalprocessor to analyze, evaluate, store, or otherwise process signalscorresponding to the light received from the different optical antennaelements 102.

In different embodiments, a computer device can be integrated with thecombiner 106, and in certain embodiments the computer device can beconfigured as a full-sized general purpose computer such as a personalcomputer (PC), a laptop, or a networked computing device. In alternateembodiments, the computer device that is included as portion of thecombiner 106 can be configured as a microprocessor, a microcomputer, anapplication-specific integrated circuit (ASIC), a devoted analog ordigital circuit, or other such device. The computer device can thereforebe configured as a general-purpose computer, a special-purpose computer,or any other type of computer that is configured to deal with thespecific task at hand. In certain embodiments, the combiner 106 includesa multiplexer and/or a downconverter that combines one or more aspectsof signals from a plurality of optical antenna elements 102 or aplurality of sets of optical antenna elements 102. While the combiner106 downconverter is presented diagrammatically herein, a number ofstructures or materials can operate as combiners, multiplexers, ordownconverters, typically through a nonlinear or linear mixing ofsignals.

Examples of signal downconverters that operate at or near opticalfrequencies are described by: J. Ward, E. Schlecht, G. Chattopadhhyay,A. Maestrini, J. Gill, F. Maiwald, H. Javadi, and I. Mehdi; “Capabilityof THz sources based on Schottky diode frequency multiplier chains”;2004 IEEE MTT-S Digest; January, 2004; pp. 1587-1590 J. Ward, G.Chattoppadhyay, A. Maestrini, E. Schlecht; J. Gill, H. Javadi, D.Pukala; F. Maiwald; I. Mehdi; “Tunable All-Solid-State Local Oscillatorsto 1900 GHz”; Dec. 22, 2004, each of which is incorporated herein byreference.

The one or more aspects of the signals can be characterized by aplurality of frequency ranges, a plurality of time samples, or aplurality of other separable or distinguishable features for the signalsthat originate from pluralities of optical antenna elements into asingle signal that can be transmitted to a remote location forprocessing, or alternatively the processing can be performed in situ.The output from the combiner 106 can be transferred to a remotelocation, such as would occur if the optical antenna assembly 100 isconfigured as part of a network. In certain embodiments of the opticalantenna assembly, a variety of components can be operably coupleddownstream or upstream of the combiner 106 to assist in the handling ortransmission of data signals produced by the combiner.

Another embodiment of a downconverter includes an optical down-converterthat, like other forms of downconverters, decreases the frequency ofsignals. One example of an optical downconverter is an optical devicethat mixes the signal to be downconverted with a second optical signal,as may be generated by an associated oscillator 107. Mixing of opticalsignals to produce a lower frequency indicator of information carried byone or more signals is known. An example of such mixing in polymer basedmaterials is described in Yacoubian, et al, E-O Polymer Based IntegratedOptical Acoustic Spectrum Analyzer, IEEE Journal of Selected Topics inQuantum Electronics, Vol. 6, No. 5 September/October 2000.

Other examples of optical downconversion using heterodyning orhomodyning are described by Yao in Phase-to-Amplitude ModulationConversion Using Brillouin Selective Side Band Amplification, IEEEPhotonics Technology Letters, Vol. 10. No. 2, February 1998;Hossein-Zadeh and Levi, Presentation at CLEO 2004, May 19, 2004,entitled Self-Homodyne RF-Optical Microdisk Receiver, each of which isincorporated herein by reference. Other approaches to downconversionand/or detection are described later in this description.

While the downconverter is shown as incorporated into the combiner, thedownconverter may be interposed between the optical antenna elements 102and the φ-adjusts 104, may be interposed between the φ-adjusts 104 andthe combiner 106, or may itself include the φ-adjusts 104. In certainembodiments, the down-converter can be operably coupled to the combiner,wherein the frequency of the electromagnetic radiation that is appliedto the combiner 106 is reduced to a level that can be propagated alongelectrical conductor. In other embodiments, it is envisioned that amixer may be applied downstream of the combiner 106.

Returning to a general description of the embodiment illustrated in FIG.1, a wavefront 120 indicates a generally planar orientation of lightwaves arriving at, and/or received by, the respective receiving opticalantenna assembly 100. While the incoming wave in this description ispresented as planar for clarity of presentation, the embodiments hereinmay be configured for operation with a variety of input wave formats,including non-coherent waves and non-planar waves. Moreover, in thedisclosure, the term “planar” as applied to waveforms is not limited tothe strictest definitions of planar and may include any substantiallyplanar surface, including those that do not have infinite radii ofcurvature or those that may, for example, have slight surfaceirregularities. For the receiving optical antenna assembly 100, thewavefront 120 is illustrated as moving in a downward direction asindicated by the arrow 124.

The receiving optical antenna assembly 100 converts the light energy ofthe wavefront 120 to electrical energy that travels along anelectrically conductive path or other signal transmissive path. Thereceiving optical antenna assembly 100 can thereby be considered as anoptical transducer that converts received light energy into a differentform.

By adjusting the relative delays of the different optical antennaelements using the φ-adjusts 104, the sensitivity, directionality, gain,or other aspects of the optical antenna assembly 100 can be controllablyvaried. In certain generating embodiments, this can provide abeamforming and/or beamsteering function.

In one approach, the φ-adjusts 104 may also be configured to selectivelyblock or diminish signals from their respective optical antenna element,as will be described below. Therefore, in certain embodiments, theφ-adjusts 104 can functionally alter the light-generating orlight-receiving effects of a particular optical antenna element 102.Removing (or decoupling) certain optical antenna elements from certainarrays of optical antenna elements can make an otherwiseregularly-spaced array more non-regularly spaced or more sparse.Alternatively, removing selected elements can functionally control thegain of the optical antenna assembly along selected paths, vary thewidth of the center lobe and/or the side lobes, or alter some othercharacteristics that may be dependent upon frequency. Designconsiderations relating to the number, position, spacing, and otheraspects of the optical antenna elements will be described hereinbelow.

In many embodiments of the receiving optical antenna assembly 100 asdescribed with respect to FIG. 1, each of the optical antenna elements102 can be configured to receive signals that vary in amplitude or phaseat different spatial directions across the array. Examples include, butare not limited to, a telescope, a camera, an image detector, areceiving portion of a facsimile machine, a communications receiver, animage copier, or the like.

Other embodiments of the receiving optical antenna assembly can bearranged to receive a substantially uniform image across the entire faceof the display. Examples of these embodiments include, but are notlimited to, motion detectors, presence detectors, time of day detectors,timing detectors associated with sports events, or the like. Theparticular configuration of the various components, such as thecombiner, can be designed to take into account the type of waveformimages that can be received by the optical antenna assembly 100, as wellas the uniformity of the waveform image.

It is envisioned that any configuration of such optical antennaassemblies that produces an electrical signal responsive to receivedlight, as claimed by the claims herein, may be within the intended scopeof the receiving optical antenna assembly.

Examples of Signal Generating Optical Antenna Elements

FIG. 2 shows a schematic diagram of one embodiment of a generatingoptical antenna assembly 100 that is configured to emit either coherentlight energy or incoherent light energy. Many of the components andtechniques that are described in this disclosure with respect toreceiving optical antenna assemblies also apply to the generatingoptical antenna assemblies, and vice versa. Different embodiments of thegenerating optical antenna assembly 100 can be used in a variety ofapplications that include, but are not limited to a light source, adisplay, and/or a variety of other applications that involve directinglight toward spatial-locations relative to that array.

In this disclosure, the receiving and generating embodiments of theoptical antenna assembly 100 can be provided with many identicalreference characters since many of the components of both configurationsmay be identical or similar, and in some cases, both configurations mayactually be used interchangeably. However, certain components of thegenerating optical antenna assembly may be configured differently forthe remaining optical antenna assembly (e.g., such as having differingcircuitry and/or different biasing) to provide for different operationalcharacteristics.

While one embodiment of the optical antenna assembly 100 may beconfigured to generate coherent radiation at certain locations similarlyto laser or holographic devices, other embodiments of the opticalantenna assembly may produce incoherent light. Such a light source couldbe steerable and controllable to produce coherent or incoherent light atdifferent times and or different spatial locations or along selectedpaths. In certain embodiments of the optical antenna assembly 100, theplurality of optical antenna elements 102 included within the generatingoptical antenna assembly 100 can be arranged in an array. In otherembodiments, the optical antenna assembly 100 may include one, or anumber of, discrete optical antenna elements 102. Each optical antennaelement 102 can be individually attached or operably coupled via adistinct φ-adjust 104.

The embodiment of the generating optical antenna assembly 100, asdescribed with respect to FIG. 2, includes the one or more opticalantenna elements 102, corresponding φ-adjusts 104, the electricalconductors 105, and signal splitter 205. The signal splitter 205diagrammatically represents a component or set of components thatdistribute signals among the various optical antenna elements 102.However, one skilled in the art will recognize that the signal splitter205 may actually include functions such as signal combining in someembodiments. For example, as described for some embodiments herein, andas represented in FIG. 2, the signal splitter 205 may combine selectedsignals with signals from an associated oscillator 206.

In one embodiment, the signal splitter 205 outputs an electrical signalthat is a combination of an information signal and the signal from theoscillator 206. The output signal travels along the electrical conductor105 to the φ-adjust 104. The φ-adjust 104 produces a phase adjustedversion of the signal to drive the respective optical antenna element102. The output of the optical antenna element 102 thus corresponds tothe information signal and the oscillator signal.

Depending upon the embodiment of the generating optical antenna assembly100, a varying, or consistent, level of illumination can be createdacross all of the optical antenna elements 102 within the opticalantenna assembly 100. For example, if the optical antenna assembly 100is configured as a light source, then each of the optical antennaelements 102 may generate relatively broadband light at its respectivespatial location. In other light source approaches the optical antennaelements 102 may be matched to selectively produce light in one or morenarrow bands or one or more substantially discrete frequencies. Wherethe light is in one or more narrow bands, the optical antenna elements102 may be sufficiently matched to generate coherent light energy.

In certain display device embodiments, it may be desirable to provide avarying light configuration across the optical antenna assembly 100 todisplay an image by varying the amplitude and/or phase of light fromrespective ones or sets of optical antenna elements 102.

If the optical antenna assembly 100 is configured as an optical display,then the intensity of the signal from each of the optical antennaelements 102 may be controlled on an individual element basis oraccording to groupings of elements to provide controllable illuminationat respective spatial locations. Where the pattern of the illuminationmatches a selected image, the emitted light energy may produce aviewable display. In some approaches, the optical antenna elements 102may be configured to emit light at one or more visible wavelengths sothat viewable image may be directly viewable or viewable on an imagesurface, such as a screen or diffuser. In other approaches, the emittedlight may be at frequencies not directly viewable by humans andconverted to visible light through wavelength conversion. In one simpleapproach to wavelength conversion, the emitted light strikes a phosphor,which may be upconverting or downconverting depending upon theconfiguration, and the phosphor emits visible light with an energy levelcorresponding to the to level of the emitted non-visible light.

Where the light emitted by the optical antenna elements 102 is coherent,the gain may be controlled as described herein to directionally controlbeam gain, to produce a scanning beam display.

As described with respect to the FIG. 1 receiving configuration of theoptical antenna assembly, the φ-adjusts 104 effectively adjust therelative transit time for a signal (in either direction) between therespective optical antenna element 102 and the corresponding signalsplitter 205. In the generating configuration of the optical antennaassembly 100, the φ-adjust 104 can thereby alter the relative phase ofthe light that is generated by the respective generating optical antennaelements. Such phase control may allow the generating optical antennaassembly 100 to act as a beamsteerer and/or beamformer to control thedirectionality or angular gain relative to the array of optical antennaelements 102.

In the embodiment of the optical antenna assembly 100 as described withrespect to FIG. 2, the oscillator 206 generates an electrical or opticalsignal that can be supplied to the respective optical antenna element102. If the signal that is generated from the oscillator 206 is anelectrical signal, the signal may directly drive the optical antennaelement 102 or the frequency may be lower than that to be emitted by theoptical antenna element 102. In such configurations, an up-converter, aswill be described below, can convert the frequency of the electricalsignal into the frequency of the light from each optical antennaelement. Signals output from each oscillator 206 can therefore beapplied to one or more respective φ-adjusts 104 that are associated witheach generating optical antenna assembly 100. Each φ-adjust 104 may thenadjust the relative phase of the light to be generated by eachrespective optical antenna element 102. As such, each φ-adjust 104 actsas a variable delay element for signals applied to the optical antennaelement 102.

The signal splitter 205 is shown in FIG. 2 as being associated with theoscillator 206. Some embodiments of the optical antenna assembly 100 usean oscillator 206 to generate a signal, that may be sinusoidal, of aparticular frequency that may then form a reference or carrier signal.The oscillator 206 can be configured in a number of differentembodiments, as described below with respect to FIGS. 11, 12, and 13. Itis emphasized that the different embodiments of the oscillator asdescribed in this disclosure are illustrative in nature, and are notintended to be limiting in scope. As such, other embodiments ofoscillators can be considered to be within the intended scope of thepresent disclosure.

In certain light-generating embodiments such as a light source, a singleoscillator 206 can generate a signal, which may be sinusoidal, that canbe applied to individual, multiple, or all of the optical antennaelements 102 within the optical antenna assembly 100. In alternateembodiments such as a display, each of the array of display pictureelements (pixels) may be defined by one or more optical antenna elements102, such that each of (or each group of) the optical antenna elements102 is associated with a distinct oscillator 206. If substantiallyuniform levels of illumination are to be provided across multipleoptical antenna elements, then fewer oscillators 206 that each supply aconsistent signal to multiple optical antenna elements may be used.

In those embodiments of the generating optical antenna assembly 100 thatdistribute a substantially uniform levels of light across an entirearray (such as where the generating optical antenna assembly 100 is usedas a light source), the signal splitter 205 can be configured with oneoscillator circuit which applies an identical input signal to each ofthe generating optical antenna elements 102.

As noted previously, in some approaches the signal splitter 205 isfunctionally configured to split an input signal, such as theinformation signal into two or more output signals that may beidentical. Each of the output signals drive a respective generatingoptical antenna element 102 or may form a carrier signal that may becombined with another signal (such as a signal from the oscillator 206)to drive the respective optical antenna element 102.

Such an embodiment may still employ φ-adjusts 104. In one approach, eachφ-adjust 104 adjusts the time for the oscillator's signal to reach thecorresponding optical antenna element 102, and therefore the relativephase of that optical antenna element. The φ-adjusts 104 in thegenerating configuration of their respective optical antenna elements102 and thereby alter the phase of the light generated across the arrayof elements within the optical antenna assembly 100. Such phase controlcan employ known techniques to control the effective direction ofemitted energy for localized or directional illumination.

Certain embodiments of the generating optical antenna assembly 100 mayinclude an up-converter that is associated with the signal splitter 205.The up-converter acts to transition light to the frequency of a receivedelectrical signal, such as may be modulated according to informationcontent into a signal at optical frequencies. Such an up-converter istypically a non-linear, square law or similar device that produces anoutput that is a function of the information bearing signal and a secondsignal, such as may be provided by the oscillator 206. An example of anon-active form of up-converter can be found in T. J. Yen, W. J.Padilla, N. Fang, D. C. Vier, D. R. Smith, J. B. Pendry, D. N. Basov, X.Zhang; “Terahertz Magnetic Response from Artificial Materials”; ScienceMagazine Reports; Mar. 5, 2004; pp. 1494-1496; Volume 303; which isincorporated herein by reference.

Other embodiments of the generating optical antenna assembly 100 includean oscillator that generates signals at optical frequencies directly,thereby bypassing the need for a separate up-converter.

It is also envisioned in certain embodiments that a mixer circuit,multiplier, nonlinear circuit, or other suitable frequency conversionconfiguration, can up-convert or downconvert the frequency of theelectrical signal that is to be transmitted or received by the signalcombiner 205 from optical frequencies to frequencies that may be handledmore easily by conventional circuitry. An example of a device thatgenerates harmonics of an input signal is described in the article: S.Takahashi, A. V. Zayats; “Near-field second—harmonic generation at ametal tip apex”; Applied Physics Letters; May 13, 2002; pp. 3479-3481;Volume 80, Number 19; American Institute of Physics, incorporated hereinby reference.

It is envisioned that any configuration of optical antenna assembly thatgenerates light in response to a received electrical signal, as claimedby the claims, may be within the intended scope of the generatingoptical antenna assembly.

Examples of Optical Antenna Assembly Fabrication Techniques

Many embodiments of the optical antenna elements 102 can be minute (inthe micro- or nano-scale), since they can have similar physicaldimensions to integer multiples or divisors of the wavelength, λ, of thelight with which the optical antenna elements couple (e.g., λ, λ/2, orλ/4). As such, each receiving or generating optical antenna element 102,as described with respect to the respective FIG. 1 or 2, is configuredto respectively receive light or generate light within the visible aswell is near-visible light spectrum. Typically, visible wavelengths areon the order of 400-700 nm. In many cases, near visible wavelengths canbe considered to be from about 300 nm up to about 1,900 nm. However,other optical ranges may be applicable. For example, the principles andstructures described herein may be extended in some cases tosubstantially shorter wavelengths, such as those of knownphotolithographic techniques. Such wavelengths can be currently on theorder of a few tens of nanometers, e.g., 40 nm, although futureproduction techniques can be expected to reduce these to the singlenanometer ranges, or even smaller. The principles herein should beadaptable to such dimensions, taking nanoscale effects into account.Similarly, the upper wavelength (lower frequency) limits are notnecessarily limited to visible or near visible wavelengths. In fact, theprinciples, structures, and methods herein may be applicable atwavelengths in the near infrared (e.g., about 700-5000 nm), mid-infrared(e.g., about 5000 nm-25 micron), or far infrared (e.g., about 25-350micron ranges). One skilled in the art will recognize that these rangesare approximate. For example, the upper end of the mid-infrared range issometimes defined as about 30 or 40 microns and the upper end of the farinfrared is sometimes defined as about 250 microns.

A quarter-wave optical antenna element 102 has an effective lengthsubstantially equal to one-quarter the wavelength of thereceived/generated light for the corresponding medium. A half-waveoptical antenna element 102 has an effective length substantially equalto one-half the wavelength of the received/generated light, for thecorresponding medium. One skilled in the art will recognize that thewavelength depends upon the configuration and associated media,including the effective dielectric constant of the media through whichthe signals propagate.

The individual optical antenna elements 102 can be arranged in arrays toform the optical antenna assemblies, and hence the optical antennaelements may be fabricated within the nano- or micro-scale. It istherefore envisioned that many optical antenna assembly applicationswill involve a large number of the optical antenna elements that can bearranged in an array. As such, one fabrication approach employssemiconductor processing techniques to produce a number of elementshaving well controlled positioning and/or dimensions.

Such fabrication approaches may be selected in cases where there arelittle operation and configuration variations between the individualoptical antenna elements, though other systems may also employ suchtechniques.

Appropriate semiconductor processing techniques include, but are notlimited to, lithography (such as photo-lithography, e-beam lithography),nanotube growth, self assembly, or fabrication of other nano structures.Other known techniques that can be used to produce large arrays ofoptical antenna elements can be within the intended scope of the presentdisclosure.

The different embodiments of the optical antenna assembly 100 cantherefore be considered as an optical antenna that “captures” or“generates” light energy, as described respectively with respect toFIGS. 1 and 2. As may be noted from the above description, phase controlof the individual optical antenna elements may allow the gain of theoptical antenna assembly to be defined independently of conventionaloptical focusing or processing techniques, such as with lenses, or ofdiffractive, refractive, or reflective elements, including left handedmaterials. However, the principles, structures, and methods describedherein do not necessarily exclude use with more conventional opticalfocusing, shaping, processing or other techniques, such as lenses,diffractive elements, phase plates, filters, apertures, polarizers, orother more conventional components or systems.

Typical analysis of photon emitters or receivers traditionally has beenconsidered under the domain of quantum physics, as often characterizedby Schroedinger's equations. While such analysis may be applicable tomany aspects of the devices and systems described herein, the design andcharacteristics of the optical antenna assembly 100 will typicallyinvolve more Maxwellian analysis and design. As such, many of theantenna techniques and equations that apply to antenna design, wavepropagation, coupling, and other aspects of the microwave, and other,electromagnetic radiation spectra may be applied relatively directly tothe designs and systems described herein. For example, optical antennaassembly designs, concepts and analysis may use phased-array techniquesfor synthetic apertures or other antenna-related concepts to detect,generate, direct, or otherwise interact with energy at opticalfrequencies.

FIG. 3 shows diagrammatically a side view of one generalized embodimentof the optical antenna assembly 100 as described with respect to FIGS. 1and/or 2. The optical antenna assembly 100 can be fabricated using avariety of semiconductor processing techniques or other suitabletechniques. In certain embodiments, the substrate 202 or supporting bodycarries such elements as the φ-adjust 104, the combiner 106, the signalsplitter 205, or the oscillator 206 as described in either FIG. 1 orFIG. 2, though these are omitted from FIG. 3 for directness ofpresentation. In this disclosure, the term “carries” in the physical,rather than signal carrying, context may apply to a component, such asthe optical antenna element, being individually attached or operablycoupled to the substrate 202, integrated into or contained within thesubstrate, operably coupled to some intermediate structure that attachesthe optical antenna element to the substrate, or any other type ofarrangement where the substrate can be said to carry or support.Additionally, in certain embodiments, the substrate 202 can beconfigured considerably differently than conventional semiconductorsubstrates. For example, materials such as polymers, metals, rubber,glasses, or minerals can form the substrate that carries the opticalantenna elements. Additionally, in certain embodiments, some type offield can be established to maintain the optical antenna element inposition with respect to each other in addition to or independent ofphysical structural support.

The substrate may also include additional components in someconfigurations, such as up-converters, down-converters, mixers, and/orde-mixers that are described with respect to certain of the figures). Arow of optical antenna elements 102 may be positioned behind or besideeach optical antenna element 102 shown in FIG. 3, thereby creating atwo-dimensional array of optical antenna elements 102.

Where the elements 102 can be positioned in a relatively stackedarrangement, multiple substrates, or one or more layers formed onsubstrates that each contain a two-dimensional array of optical antennaelements can be positioned in fixed or variable positions relative toeach other. In some cases, the two dimensional arrangements can beaccomplished by variable spacing between the rows of optical antennaelements 102 or other non-uniform arrangements. Such two dimensionalarrangements may be stacked, deposited, formed or otherwise assembled orfabricated with a stacked, layered, or other three dimensionalarrangement to form a three-dimensional array of optical antennaelements. Such three-dimensional arrays can be used for a variety ofpurposes, for example as a group of cooperating optical antennaelements.

In other applications, one or more of the layers of optical antennaelements may operate as a reference waveform generator. The referencewave may provide a driving signal for down converting or mixing, mayoperate as a relative phase control, or may provide a reference waveagainst which incoming or outgoing waves can be compared. In oneapproach, the energy of the reference wave may be applied simultaneouslywith that of an incoming wave to produce an electrical signal thatcorresponds to a linear or nonlinear combination of the incoming andreference waves. In one relatively straightforward approach, theelectrical signal corresponds to the sum of the amplitudes of thereference wave and the incoming wave. If the two waves are atsubstantially the same frequency, the sum may be a coherent sum andprovide relative phase information.

A variety of arrays of non-regular or regular optical antenna elementconfigurations can be described with respect to this disclosure. In oneembodiment, spacing between each row and/or column of optical antennaelements 102 is relatively uniform to produce regular arrays of opticalantenna elements 102. Alternatively, each one of the optical antennaelements may be irregularly spaced to produce relatively non-uniformarrays of optical antenna elements. A variety of regular or irregulararrays of optical antenna elements can be selected depending upon thedesired antenna gain and beam pattern. Where the relative phases ofincoming or outgoing waves can be determined or controlled, the gain ordirectionality of the optical antenna assembly can be controlled usingbeamforming and beamsteering concepts. The design, material, or theconfiguration of the optical antenna elements may be selected based uponthe particular design or application of the array of the optical antennaelement.

In one embodiment, lithographical approaches can produce a large numberof different embodiments of arrays of optical antenna elements 102, ordiscrete optical antenna elements. The complexity of each opticalantenna element ranges from relatively simple dipole optical antennaelement configurations, including for example, nanotubes or conductiveor dielectric pillars, to those including bends, curves,discontinuities, or other irregular configurations. Lithographictechniques can be used to pattern the optical antenna elements or otherparts of the optical antenna assembly into a more complex shape to form,for example, curves, angles, or discontinuous structures such as may beused to produce impedance matching structures, phase control structures,diodes, transistors, capacitive structures, inductive structures,resistive structures, vias, or other structures, including those thatcan be more complex or include combinations of such structures. As oneexample, nanotube-based structures have been developed with integralbends that have been shown to be capable of providing nonlinearelectrical responses. Such structures may act simultaneously as opticalantenna elements and nonlinear devices. Lithographic techniques cantherefore be used to repetitively produce a number of arrays of similaror dissimilar components quickly and accurately.

In a typical photolithographic process, a protective photoresist layeris deposited atop a substrate or other planar object that is formed froma semiconductor material or metal. The photoresist layer is patternedsuch as is generally known, with a variety of photo-based developmentprocesses. An exposed portion of the material is then etched orotherwise removed, for example, through ion beam or e-beam milling.While this embodiment of a process is disclosed herein, a number ofother fabrication techniques may be appropriate. For example, directe-beam lithography, lift-off techniques, nanogrowth or other techniquesmay be selected, depending upon the particular configuration,application, dimensions, or other factors.

FIG. 4 shows an embodiment of an optical antenna assembly 100, in whichring shaped optical antenna elements 102 are formed on the substrate 202using lithographic techniques, such that the materials may be depositedaccording to known techniques. Deposition may be appropriate in avariety of configurations, including those where the optical antennaelements 102 can be on the order of some fraction of the wavelength ofthe incoming or outgoing light.

While the optical antenna elements 102 of FIG. 4 are presented as ringshaped, other geometric or non-geometric shapes may also be selected.

In one embodiment, each optical antenna element 102 may be formed withmetals as gold, silver, aluminum, or copper. The antenna elementmaterial may be provided, for example, by electrochemical deposition,physical-vapor deposition, chemical vapor deposition, or may be grown ina variety of manners. In certain embodiments, the optical antennaelements may also be formed from semiconductor or similar materials suchas carbon or silicon based materials that can be typically doped orotherwise combined with additional materials. In one embodiment, themetal and/or semiconductor materials of the optical antenna element canbe selected to have a relatively high electron mobility. High electronmobility materials have been developed to operate at relatively highfrequencies. For example, terahertz band high electron mobility deviceshave been reported.

Minimum achievable dimensions of features produced by semiconductor orsimilar fabrication techniques are steadily decreasing. The currentlevel of dimensions can produce many embodiments of the optical antennaelements. For example, integrated circuit manufacturers have releasedcommercial devices with dimensions below 100 nm and have announced plansfor dimensions to a few tens of nanometers. It is expected that theprecision, dimensional control, manufacturability and other aspects ofthe structures and methods described herein may benefit from suchtechnological developments. Such technological developments may beexpected to produce optical antenna elements having dimensions on theorder of a few tens of nanometers. In some cases, optical antennaelements can have high vertical aspect ratios, for example 10:1 orgreater A dipole optical antenna element, or a non-regular antenna, of700 nm, 350 nm, or 175 nm is therefore realizable using currenttechnologies.

Another technique that can be used to generate a number of embodimentsof optical antenna elements is e-beam lithography. Using e-beamtechniques, the user can precisely control the shape and dimensions of afeature that is being produced. Many embodiments of e-beam techniquesprovide for higher precision than current lithographic techniques, andprovide for forming features having dimensions down to a couple ofnanometers. As such, there can be a variety of techniques to form anarray of minute optical antenna assemblies. One relativelystraight-forward technique involves fabricating the optical antennaelements as metal lines on a substantially uniform semiconductor siliconsubstrate, or alternatively on a complex substrate such as asilicon-on-insulator (SOI) substrate, a silicon-on-sapphire substrate, asilicon-on-diamond substrate, or any other suitable configuration ofsubstrate (or other item that is configured to maintain the relativeposition of the optical antenna elements) using conventionalsemiconductor manufacturing approaches. Other materials, includingsemiconductors, dielectrics, or conductors can form the substrate.

FIGS. 5 a and 5 b show one embodiment of the optical antenna assembly100, including each of a plurality of nanotubes that form the array ofoptical antenna elements 102 as carried by the substrate 202. Opticalantenna assemblies can include a large number and variety ofconfigurations of optical antenna elements, and can be formed asdipoles, curved structures, discontinuous structures, etc. can be grownusing carbon-based nanostructure technology (e.g., using carbon-based orother nanotubes). A large number of nanotubes can be grown to form anarray of optical antenna elements using nano-structure techniques by,for example, having minute depressions initially being formed as apattern upon a substrate using such techniques as lithography. Thelocations of the one or more depressions correspond to the desiredlocations of the nanotubes to be grown. The patterned substrate is thenlocated in a deposition chamber for as long as desired depending uponthe length of the nanotubes. The locations of the patterned depressionscan be referred to in this disclosure as “seed regions” 504 since thenanotubes can be selectively grown at the location of the patterneddepressions. Typically, nanotubes form as thin structures, ranging fromone to tens of molecules in diameter for different embodiments of thenanotubes. While the exemplary embodiment herein is described asincluding ones to tens of molecules, in some applications, nanotubediameters may exceed such dimensions.

In the nanotubes, each optical antenna element 102 may be grown at thelocation of a defect in a substrate. In certain embodiments, thenanotubes can be grown at an angle with respect to the surface(including parallel to the surface). Each optical antenna element canhave different, or even random, angular orientation with respect to thesurface of the substrate. In different embodiments, each nanotube can befabricated straight, or fabricated as having some curvature. In thisdisclosure, the curvature can be considered as a non-regular antennaconfiguration that is differentiated from the regular dipole antennaconfiguration. The duration of growth and the rate of growth determinethe resulting desired height, angle, and curvature of each nanotube.

In certain embodiments, certain nanotubes can be even crossed or crossedand joined to form an intersection point. As such, if a nanotube of aparticular height is desired to be formed, then the nanotube can beallowed to grow for a prescribed time duration corresponding to thatlength and rate of growth. Such approaches have been applied to producenonlinear devices such as transistors, diodes, and field emissionstructures, as described for example in M. Ahlskog, R. Tarkiainen, L.Roschier, and P. Hakonen, Single-electron transistor made of twocrossing multiwalled carbon nanotubes and its noise properties, AppliedPhysics Letters Vol 77(24) pp. 4037-4039. Dec. 11, 2000; and Cumings andZettl, Field emission and current-voltage properties of boron nitridebased field nanotubes,

FIG. 5 b shows a top view of one embodiment of the nanotubes as shown inFIG. 5 a. Multiple nanotubes that form an array can be grown to auniform height, or different heights, as desired. Many embodiments ofthe nanotubes can be carbon-based, although any suitable material thatcan be used and is within the intended scope of the present disclosure.

The array of the optical antenna elements 102 as described with respectto FIGS. 5 a and 5 b can therefore be arranged in a one-dimensional,two-dimensional, or three dimensional nano-structure pattern, and may beeither formed in a regular or an irregular pattern. The embodiments ofoptical antenna elements 102 that are described with respect to FIGS. 3,4, and 5 a may be used to fabricate either the generating or receivingoptical antenna elements 102 within the respective generating orreceiving optical antenna assembly 100. A number of the differentembodiments of the patterns of optical antenna elements 102 that form anarray in the optical antenna assembly 100 are described later in thisdisclosure.

A number of nanotube-based optical antenna element fabricationtechniques can use crystalline procedures, can use polymers, or even canuse biologically inspired polymers (such as deoxyribonucleic acid (DNA)or proteins). The structure of the resulting nanotubes can becrystalline. In certain embodiments, nanotubes can be conceptuallyformed as a crystalline structure by forming a planar graph graphenesheet into a cylinder, and capping the ends of the cylinder with asemi-spherical “buckyball”. Other configurations of, and processes for,forming nanotubes or similar structures can also be within the intendedscope of the present disclosure. The crystalline approaches (including,but not limited to, nanotubes and other nano-structures) might be moresuitable to optical antenna elements that can be arranged in a patternperpendicular to the plane formed by the waveform, either for agenerating or receiving optical antenna element. There can be, however,also a number of different configurations of antenna design. Manyoptical antenna assembly designs can leverage existing knowledge ofoptical systems that operate, for example, in the microwave ormillimeter range. Depending on the particular embodiment, such opticalantenna assemblies could be applied to either broadband or narrowbandantenna applications.

A number of different configurations of receiving optical antennaassembly configurations can operate as detectors. One embodiment of theoptical antenna assembly simulates human vision by providing threearrays of tuned optical antenna elements, with each one of the threearrays being optimized or tuned for operation at the light frequenciesthat is particularly detectable by human vision (red, green, and bluewavelengths of light). Each of the three arrays of optical antennaelements can be formed as a distinctive ring. For example, in oneembodiment of an optical antenna assembly, three arrays of opticalantenna elements 102 form three concentric ring arrays (or other shapesof arrays) that can each be configured/colored as red, green, and bluelight-receiving rings (not shown).

While the above describes an embodiment of the receiving optical antennaassembly that detects a plurality of light frequencies corresponding tocolors such as red, green, and blue; it is also within the intendedscope of the present disclosure to provide multi-colored generatingoptical antenna assemblies that generate or receive other ranges ofmulti-colored light. Such multi-colored generating or receiving opticalantenna assemblies may be applicable to display and projectorapplications, such as is likely for next generation television, display,projector, computer, theater, or other similar applications. In otherfrequency ranges, the multi-color or dual-color receiving or generatingoptical antenna assemblies may be configured to operate in other visiblelight ranges, or infrared or ultraviolet ranges.

Generating or receiving optical antenna assemblies may be configured togenerate/receive light of a variety of distinct frequencies, frequencyranges, or combination of frequencies or frequency ranges, whileremaining within the scope of the present disclosure. For example, itmay be desired to use optical antenna elements that can generate orreceive light in the near infrared or near ultraviolet light spectrum,as may be useful for a variety of applications, including thermalimaging, ultraviolet illumination or detection, or any other appropriateapplication. In other embodiments, it may be desired to generate/receivelight using a single frequency. Such transmission or detection mayprovide more selectivity, simplified detection, synchronous operation,and/or reduced cost or complexity. The particular light applicationshould be considered when determining the frequency of the generated orreceived optical energy.

Examples of Optical Antenna Phase Techniques

FIG. 6 displays one embodiment of signals, which may be sinusoidal,being generated by a plurality of optical antenna elements 102 a and 102b that together forms an associated signal-strength graph. FIG. 7displays one embodiment of FIG. 6 in which the highest amplitudegenerated light is beamsteered upwardly by a few degrees with respect toFIG. 6. While an array of optical antenna elements 102 would typicallyinclude a large number of elements; only two optical antenna elements102 a and 102 b are illustrated in FIGS. 6 and 7 for clarity indescribing certain beamforming and beamsteering techniques. Theseconcepts can be extended to much larger arrays of optical antennaassemblies 100. Each optical antenna element 102 a and 102 b radiatessignal patterns such as are illustrated in FIGS. 6 and 7 as respectivesignal lines 702 a and 702 b.

The respective signal lines 702 a and 702 b generated by the opticalantenna elements 102 a and 102 b are represented in the drawing as beingradiated in a generally hemispherical pattern. One skilled in the artwill recognize that the actual emission pattern from each of theelements, including amplitude and phase, may depend upon theconfiguration of the individual antenna element and on the materialsand/or structures of, surrounding, or near the individual elements.Thus, patterns other than hemispherical may be within the scope of thisdisclosure, though hemispherical is selected for clarity of presentationof the concepts herein. Further, the description of propagation andinteraction of waves herein is simplified to a case where the waves aretypically of the same wavelength. This aspect lends itself in many casesto coherent wave interaction. One skilled in the art will recognize thatvariations in frequency, differences in frequency, non-coherentconcepts, and other types of interaction and related techniques andprinciples may be applicable for certain configurations or applicationsof the methods and structures described herein.

Also, only two-dimensions of the spherical pattern of the signal lines702 a and 702 b are shown in FIGS. 6 and 7 for clarity of illustration,though typically, such configurations would be analyzed in threedimensions using known techniques for analyzing beam propagation andinterference. Each signal line 702 a and 702 b represents, for example,a crest of a sinusoidal pattern that is formed by respective opticalantenna elements 102 a and 102 b. The location where the signal lines702 a and 702 b intersect represents those phase intersection points 704where the signal lines 702 a and 702 b correspond to each other (areboth at a crest), and therefore can be in phase.

FIGS. 6 and 7 illustrate a number of phase intersection lines 706 thatpass through many of the phase intersection points 704. The largest and,typically, the strongest of the phase intersection lines 706 acorresponds to a main lobe 708 as shown in the signal strength plot.

The phase intersection lines 706 a, 706 b, and 706 c determine thelocations where waves constructively add to form amplitude peaks. Twoadditional phase intersection lines 706 b and 706 c correspond to sidelobes 710 in the signal strength plot in FIGS. 6 and 7. At any locationalong the phase intersection lines 706 a, 706 b, and 706 c, the signalsfrom both optical antenna elements 102 a and 102 b add constructively.As such, the phase intersection lines 706 a, 706 b, and 706 c typicallycorrespond to the highest light amplitude regions of the optical antennaassembly.

While FIGS. 6 and 7 present a simplified presentation of coherentinteraction, and demonstrate how formation of the main lobe 708, as wellas the side lobes 710, or the general direction of the phaseintersection lines 706 a, 706 b, and 706 c follow antenna patterntechniques and concepts, the availability of many elements and thecontrol of element positioning will often permit much more flexibilityin relative position, number, orientation, and other characteristics ofthe antenna assembly. Designs utilizing such flexibility can bedeveloped using conventional analytical or computer based techniques fordesigning or analyzing arrays of antenna elements.

Moreover, while FIGS. 6 and 7 illustrate either generating antennapatterns according to the generating optical antenna elements 102 a and102 b, such antenna pattern concepts can be also applicable to receivingoptical antenna elements. Antenna patterns, for both the generating andreceiving optical antenna elements 102 a and 102 b, correspond largelyto the relative phase and amplitude of the light-waves as indicated bythe respective signal lines 702 a and 702 b. For example, FIG. 7 showsthat changing the phases of the respective signal lines 702 a and 702 bcan change the location of the phase intersection lines 706 a, 706 b,and 706 c as well as the characteristics of the main lobe 708 and theside lobes 710 (characterized by the location, relative magnitude,width, or other features). FIG. 7 illustrates the effect of shifting thephase of the wave generated or received by the lower optical antennaelements by some amount with respect to the waves generated/received bythe upper optical antenna element.

As such, the phase of the lower optical antenna element 102 b is altered(e.g. steered ahead) with respect to the phase of the upper opticalantenna element 102 a by 180 degrees. This process of shifting the phaseof the signal that is generated by at least one of the optical antennaelements 102 with respect to another of the optical antenna elements tocontrol directionality of the optical antenna assembly is referred toherein as beamsteering for convenience, though the concept ofcontrolling the structure, direction and/or shape of the antenna patternmay be addressed in contexts other than directing a beam of energy.

One skilled in the art will recognize that other actions relative tocontrolling phase or relative phase may be directed toward other effectsas well, including possible lobe optimization, wave coupling, or othereffects. Moreover, the discussion herein has omitted the effects ofpolarization or E-field orientation to simplify the presentation of theconcepts and principles. One skilled in the art will recognize that avariety of analytical, experimental, and other techniques, as well as avariety of structures may be applied to design, implement, analyze orotherwise treat or understand polarization effects.

Beamsteering can also shift the relative positions of the main lobe 708and the side lobes 710 with respect to the optical antenna elements 102a and 102 b. Note, for example, that the main lobe 708 and the sidelobes 710 as described with respect to FIG. 7 are rotated in a generallycounter-clockwise direction when compared to FIG. 6. In a simplisticexample, increasing a gradient of the phase difference between wavesfrom different optical antenna elements increases shifting of the mainlobes and/or the side lobes. While the concept of beamsteering maybecome more computationally involved as the number of the opticalantenna elements in an array is increased, conventional approaches canstill be used.

This disclosure provides a number of embodiments of techniques by whichbeamsteering, beamforming, antenna pattern control, or other adaptiveantenna techniques can be applied to optical antenna assemblies 100.Other embodiments of beamsteering and beamforming techniques across avariety of arrays of optical antenna elements 102 may be within theintended scope of the present disclosure.

As noted above, in some applications, the optical antenna elements maybe fabricated according to photolithographic or similar techniques andmay be on the order of a portion of an optical wavelength or a fewoptical wavelengths. Consequently, in some configurations an opticalantenna assembly may include a large number, several thousand or evenmillions of antenna elements 102. Moreover, in some configurations, a1,000 by 1,000 element array may have a cross-sectional area on theorder of 1 mm by 1 mm. Such a small assembly may be useful as acomponent of a variety of light capturing devices or systems, such ascameras, copiers, scanner, optical detectors, or may be useful in manyother light capturing configurations. Additionally, components of suchsize may be useful in light emissive applications ranging fromillumination to coherent beam generation.

While compact assemblies may have inter-element spacings on the order ofa portion of a wavelength to a few wavelengths, in some applications itmay be desirable to have larger inter-element spacings. Sucharrangements with increased spacing between the optical antenna elementsmay be applied to such applications as synthetic aperture radar (SAR)systems, sparse antenna arrays, radio telescopes, or the like.

Software that has been developed for, and supports the so-called“synthetic aperture technique” and interferometric approaches. Suchsoftware can be run, for example, in association with the opticalantenna controller 1700 as described below with respect to FIGS. 20, 17,18, and 19.

Embodiments of Receiving and Modulating Approaches

In embodiments of optical antenna elements 102 that receive light asdescribed with respect to FIG. 1, it often is desired to detect orotherwise process electrical energy generated within or around one ormore of optical antenna elements 102 responsive to the optical antennaelement. In many embodiments, it may be useful to process the electricalenergy at frequencies approaching the frequency of the incident light orto process the electrical energy synchronously. While conventionalcommercial electronic devices do not typically operate synchronously atoptical frequencies, the principles upon which such devices can bedesigned and fabricated can be extensible to such frequencies, thoughmany effects, such as skin depth, that may be ignored at lowerfrequencies may become significant at such higher frequencies. In fact,such analyses are regularly presented and verified experimentally in theliterature relating to “plasmons” or “polaritons”.

Within this disclosure, the signals (in both transmitting and receivingembodiments of optical antenna assemblies) include any propagation,including polaritons and phononic. As such, in this disclosure, whenreference is made to energy traveling or propagating along an electricalpath, it is intended that the propagation can include within, adjacentto, outside of, parallel to, through, and any other known conductionmechanism relative to an electrical path.

Descriptions of surface plasmon polaritons and related structures,fabrication techniques and analyses can be found at “Terahertz surfaceplasmon polaritons”; THz SPP's; printed on Dec. 22, 2004; pp. 1-4;located at: http://www-users.rwth-aachen.de/jaime.gomez/spp.html; N.Ocelic, R. Hillenbrand; “Subwavelength-scale tailoring of surface phononpolaritons by focused ion-beam implantation”; Nature Materials-Letters;September 2004; pp. 606-609; Volume 3; Nature Publishing Group, M.Salerno, J. R. Krenn, B. Lamprecht, G. Schider, H. Ditlbacher, N.Felidj, A. Leitner, F. R. Aussenegg; “Plasmon polaritons in metalnanostructures: the optoelectronic route to nanotechnology”;Opto-Electronics Review; Dec. 22, 2004; pp. 217-224; Volume 10, Number3; G. Schider, J. R. Krenn, A. Hohenau, H. Ditlbacher, A. Leitner, F. R.Aussenegg, W. L. Schaich; I. Puscasu, B. Monacelli, G. Boreman; “Plasmondispersion relation of Au and Ag nanowires”; Physical Review B; 2003;pp. 155427-1/155427-4; Volume 68, Number 15; The American PhysicalSociety; and N. Stoyanov, D. Ward, T. Feurer, K. Nelson; “Terahertzpolariton propagation in patterned materials”; Nature Materials-Letters;October 2002; pp. 95-98; Volume 1; Nature Publishing Group; and J. P.Kottmann, Olivier J. F. Martin; “Plasmon resonant coupling in metallicnanowires”; Optics Express; Jun. 4, 2001; pp. 655-663; Volume 8, Number12, each of which is incorporated herein by reference.

Examples of surface-plasmon analysis, structures, techniques and designrelative to optical fields and propartion can be found in S.Bozhevolnyi, I. Smolyaninov; A. Zayats; “Near-field microscopy ofsurface-plasmon polaritons: Localization and internal interfaceimaging”; Physical Review B; Jun. 15, 1995; pp. 17916-17924, FIGS.3,5,7,9,11; Volume 51, Number 24; The American Physical Society; W. L.Barnes, W. A. Murray, J. Dintinger, E. Devaux, T. W. Ebbesen; “SurfacePlasmon Polaritons and Their Role in the Enhanced Transmission of Lightthrough Periodic Arrays of Subwavelength Holes in a Metal Film”;Physical Review Letters; Mar. 12, 2004; pp. 107401-1/107401-4; Volume92, Number 10; The American Physical Society; H. Ditlbacher, J. R.Krenn, G. Schider, A. Leitner; F. R. Aussenegg; “Two-dimensional opticswith surface plasmon polaritons”; Applied Physics Letters; Sep. 2, 2002;pp. 1762-1764; Volume 81, Number 10; American Institute of Physics, H.Cao, A. Nahata; “Resonantly enhanced transmission of terahertz radiationthrough a periodic array of subwavelength apertures”; Optics Express;Mar. 22, 2004; pp. 1004-1010; Volume 12, Number 6; I. I. Smolyaninov, A.V. Zayats, C. C. Davis; “Near-field second harmonic generation from arough metal surface”; Physical Review B; Oct. 15, 1997; pp. 9290-9293;Volume 56, Number 15; The American Physical Society each of which isincorporated herein by reference.

In another approach, such analyses may be applied to negative refractiveor left-handed materials, as described in R. Ruppin; “Surface polaritonsand extinction properties of a left-handed material cylinder”; Journalof Physics: Condensed Matter; Aug. 13, 2004; pp. 5991-5998; Volume 16;IOP Publishing Ltd, and T. J. Yen, W. J. Padilla, N. Fang, D. C. Vier,D. R. Smith, J. B. Pendry, D. N. Basov, X. Zhang; “Terahertz MagneticResponse from Artificial Materials”; Reports; Mar. 5, 2004; pp.1494-1496; Volume 303; Science Magazine; each of which is incorporatedherein by reference.

With polaritons, energy may considered to be propagated adjacent,internal, and/or external to a guiding surface, such as a metal,nanotube, photonic crystal, or other material.

In considering the optical antenna assembly, the relatively highfrequency of the light will impact the analysis and design. Light havinga wavelength of, e.g., 500 nm has a frequency of approximately 600 Thz,while light having a wavelength of 30 microns has a frequency of about10 THz and light having a wavelength of 300 microns has a frequency ofabout 1 THz. One skilled in the art will recognize that manycommercially available components typically used for lower frequencyassemblies may not yet be available at optical frequencies. However, asthe scale of the optical antenna elements is reduced to within one or afew orders of magnitude relative to the wavelength of the optical waves,the capacitance, inductance, and other parameters will also scale. Asoperational frequencies of available components rise, the simplicity andmanufacturability of such devices is expected to improve. More detailsregarding operation of certain embodiments of such components arediscussed below with reference to mixing.

Moreover, several techniques are becoming available for integratingelectronic or non-linear features into the optical antenna assembly. Asnoted above, for example, carbon nanotubes having diode-like featureshave been reported. Similarly, a number of nonlinear devices, such astransistors, have been integrated in or analyzed in conjunction withmicro- or nanoscale structures such as nanotubes, and in some cases havebeen described as operating at terahertz ranges. Example techniques anddescriptions can be found in the Ahlskog and Cumings referencesdescribed above as well as:

J. U. Lee, P. P. Gipp, C. M. Heller; “Carbon nanotube p-n junctiondiodes”; Applied Physics Letters; Jul. 5, 2004; pp. 145-147; Volume 85,Number 1; American Institute of Physics; C. Lu, Q. Fu, S. Huang, J. Liu;“Polymer Electrolyte-Gated Carbon Nanotube Field-Effect Transistor”;Nano Letters; Mar. 12, 2004; pp. 623-627; Volume 4, Number 4; AmericanChemical Society; J. Guo, M. Lundstrom, S. Datta; “Performanceprojections for ballistic carbon nanotube field-effect transistors”;Applied Physics Letters; Apr. 29, 2002; pp. 3192-3194; AmericanInstitute of Physics; Z. Yao, H. W. C. Postma; L. Balents; C. Dekker;“Carbon nanotube intramolecular junctions”; Letters to Nature; Nov. 18,1999; pp. 273-276; Volume 402; Macmillan Magazines Ltd.; J. Guo, S.Datta, M. Lundstrom; “A Numerical Study of Scaling Issues for SchottkyBarrier Carbon Nanotube Transistors”; School of Electrical and ComputerEngineering—Purdue University; printed on Dec. 22, 2004; pp. 1-26; A.Javey, J. Guo; M. Paulsson, Q. Wang, D. Mann, M. Lundstrom, H. Dai;“High-Field Quasiballistic Transport in Short Carbon Nanotubes”;Physical Review Letters; Mar. 12, 2004; pp. 106804-1/106804-4; Volume92, Number 10; The American Physical Society; A. Javey, J. Guo, D. B.Farmer, Q. Wang, E. Yenilmez, R. G. Gordon, M. Lundstrom, H. Dai;“Self-Aligned Ballistic Molecular Transistors and Electrically ParallelNanotube Arrays”; Nano Letters; Jun. 23, 2004; pp. 1319-1322; Volume 4,Number 7; American Chemical Society; A. Javey, J. Guo, D. B. Farmer, Q.Wang, D. Wang, R. G. Gordon, M. Lundstrom, H. Dai; “Carbon NanotubeField-Effect Transistors with Integrated Ohmic Contacts and High-k GateDielectrics”; Nano Letters; Feb. 20, 2004; pp. 447-450; Volume 4, Number3; American Chemical Society; J. Guo, J. Wang, E. Polizzi, S. Datta,Mark Lundstrom; “Electrostatics of Nanowire Transistors”; School ofElectrical and Computer Engineering-Purdue University; printed on Dec.22, 2004; pp. 1-23; A. Javey, J. Guo, Q. Wang, M. Lundstrom, H. Dai;“Ballistic carbon nanotube field-effect transistors”; Nature; Aug. 7,2003; pp. 654-657; Volume 424; Nature Publishing Group; J. Guo, S.Goasguen, M. Lundstrom, S. Datta; “Metal-insulator-semiconductorelectrostatics of carbon nanotubes”; Applied Physics Letters; Aug. 19,2002; pp. 1486-1488; Volume 81, Number 8; American Institute of Physics;S. Li, Z. Yu, S. Yen, W. C. Tang, P. J. Burke; “Carbon NanotubeTransistor Operation at 2.6 GHz”; Nano Letters; Mar. 23, 2004; pp.753-756; Volume 4, Number 4; American Chemical Society; I. Y. Lee, X.Liu, B. Kosko, C. Zhou; “Nanosignal Processing: Stochastic Resonance inCarbon Nanotubes That Detect Subthreshold Signals”; Nano Letters; Nov.11, 2003; pp. 1683-1686; Volume 3, Number 12; American Chemical Society;each of which is incorporated herein by reference.

An example of one detector is described in W. Knap, Y. Deng, S.Rumyantsev, and M. S. Shur; “Resonant detection of subterahertz andterahertz radiation by plasma waves in submicronfield-effecttransistors”; Applied Physics Letters; Dec. 9, 2002; pp. 4637-4639;Volume 81, Number 24; American Institute of Physics; and in J. Ward, F.Maiwald; G. Chattopadhhyay, E. Schlecht, A. Maestrini, J. Gill, I.Mehdi; “1400-1900 GHz Local Oscillators for the Herschel SpaceObservatory”; Dec. 22, 2004; each of which is incorporated herein byreference.

Antenna elements with integrated nonlinear devices can operate as eitheror both of optical antenna elements 102 and mixers. In one mixing-typeof approach, the electrical energy may be mixed or otherwise compared toa second electrical signal produced in response to a reference opticalsignal. In some approaches, such as heterodyning, a high frequencysignal is mixed with a reference signal in a nonlinear device, such as adiode or transistor to produce signals having a frequency correspondingto a difference between the high frequency signal and the referencesignal. In one approach the reference signal is generated with a localoscillator, according to techniques such as those described for examplein A. Maestrini, J. Ward, J. Gill; G. Chattopadhyay, F. Maiwald, K.Ellis, H. Javadi, I. Mehdi; “A Planar-Diode Frequency Tripler at 1.9THz”; 2003 IEEE MTT-S Digest; January 2003; pp. 747-750; J. Ward, G.Chattoppadhyay, A. Maestrini, E. Schlecht; J. Gill, H. Javadi, D.Pukala; F. Maiwald; I. Mehdi; “Tunable All-Solid-State Local Oscillatorsto 1900 GHz”; Dec. 22, 2004, each of which is incorporated herein byreference.

In some applications, information content of the optical signal may bedetected synchronously, through optical or electrical approaches. In oneoptical approach, an optical reference signal is applied to one or moreantenna elements to produce a reference electrical signal.

The reference electrical signal and the electrical signal correspondingto the received optical signal can be mixed, in a nonlinear or similarsignal processing device, such as a transistor, diode, or bolometer toproduce a downconverted signal component that may be processed further.As noted previously, the nonlinear device may be integral to orintegrated with the optical antenna elements 102.

In some approaches, it may be adequate to process incoming opticalenergy without specific phase information. In one such approach, theantenna elements 102 convert incoming optical energy to electricalenergy and the electrical energy is integrated or accumulated over sometime duration. An example of a radiation detector that uses thebolometer effect is described in the article: G. N. Gol'tsman, A. D.Semenov; Y. P. Gousev; M. A. Zorin; I. G. Gogidze; E. M. Gershenzon; P.T. Lang; W. J. Knott; K. F. Renk; “Sensitive picosecond NbN detector forradiation from millimetre wavelengths to visible light”; Supercond. Sci.Technol.; 1991; pp. 453-456; IOP Publishing Ltd, which is incorporatedby reference as well as in other references previously incorporatedherein.

In one approach, the accumulated electrical energy can be detected usingconventional electronic techniques. In other approaches, electricalenergy can be detected and/or measured using photonic techniques similarto those described in G. Schider, J. R. Krenn, A. Hohenau, H.Ditlbacher, A. Leitner, F. R. Aussenegg, W. L. Schaich; I. Puscasu, B.Monacelli, G. Boreman; “Plasmon dispersion relation of Au and Agnanowires”; Physical Review B; 2003; pp. 155427-1/155427-4; Volume 68,Number 15; J. R. Krenn; “Nanoparticle Waveguides Watching energytransfer”; News & Views; April 2003; pp. 1-2; Volume 2; NatureMaterials; or Nature Materials-Letters; September 2004; pp. 606-609;Volume 3; Nature Publishing Group, each of which is incorporated hereinby reference.

As noted previously, different embodiments of the signal processingcomponents that can be associated with each optical antenna element canbe configured as diodes, transistors, or other components as describedin this disclosure. In the FIG. 8 embodiment, the optical detector 804is configured as a diode 808. There can be variety of embodiments ofdiodes 808 that can be used. In FIG. 8, the diode 808 is representedconventionally with a p-region 810 that is positioned adjacent to ann-region 812, though a variety of structures may be applicable. Suchp-regions 810 and n-regions 812 are typically formed by doping accordingto known techniques. One skilled in the art will recognize that otherdiode or other nonlinear structures may be appropriate for certainapplications. For example, planar diode multipliers, Schottky diodes,field emission devices, and HEMT devices are described hereinbelow andin various references incorporated herein. In many cases the particularcomponent may be designed specifically to interact with its respectiveone or more optical antenna elements 102.

For example, in many embodiments, the magnitude of the electrical signalproduced by the one or more of the optical antenna elements 102corresponds to the amplitude of the optical wave interacting with it. Insome applications, the electrical signal will propagate in a mannercorresponding to its frequency and the structure of the optical antennaelements 102 and the electrical conductor. For example, where theelectrical signal is at very high frequencies, it is likely to becarried in the form of a plasmon. The plasmon is guided by theelectrical conductor or by the optical antenna element to, or near, thenonlinear component, where the plasmon may produce a change in anelectric field in, around, adjacent to or otherwise interacting with thecomponent. The component responds to the interaction by producing acorresponding output electrical signal. A variety of interactingapproaches may be applicable.

The optical antenna elements and their associated signal processingcomponents, as described with respect to FIGS. 8 and 9, may include anonlinear device such as a diode or transistor integrated with orcoupled to optical antenna elements. As shown in a diagrammaticrepresentation in FIG. 8, the n-region 812 of diode 808 carries anoptical antenna element 102. The n-region 812 is integrated into asubstrate 202 that includes a p-region 810. As is known adjoining n andp-regions can form a diode, thus forming a nonlinear device. As is alsoknown, nonlinear devices, such as diodes can form portions ofrectification or signal processing circuitry. While the diagrammaticrepresentation of FIG. 8 shows the diode being physically discrete fromand carrying the optical antenna element 102, the diode may beincorporated into the diode as is noted hereinbelow. Moreover, althoughthe representational diode 808 of FIG. 8 includes a pn-junction, otherconfigurations, such as those including Schottky diodes may be moreappropriate in some configurations. Such diodes and integration withwaveguides, nanotubes, and other components are referred to hereinbelowand in several of the references incorporated herein by reference.

In a transistor type of implementation presented in FIG. 9, an opticaldetector 804 that responds to the electrical signal induced in theoptical antenna element 102 includes a transistor 908. The embodiment oftransistor 908 that is described with respect to FIG. 9 is afield-effect transistor (FET), as indicated by the identity of theterminals (a source 910, a gate 912, and a drain 914), though othertransistor configurations may be appropriate in some configurations, asnoted below.

In this embodiment, the optical antenna element 102 is coupled to thegate 912 and the source 910 and drain 914 can be biased in aconventional manner. The details of biasing and other electroniccircuitry can be represented diagrammatically, as the details of theelectronic circuitry will depend upon the application, frequency, andconfiguration. Specific examples of electronic circuitry coupled totransistor-like elements at far infrared frequencies are reported forwaves arriving at an antenna structure in J. C. Pearson, I. Mehdi, E.Schlecht, F. Maiwald, A. Maestrini, J. Gill, S. Martin, D. Pukala, J.Ward, J. Kawamura, W. R. McGrath, W. A. Hatch, D. Harding, H. G. Leduc,J. A. Stem, B. Bumble, L. Samoska, T. Gaier, R. Ferber, D. Miller, A.Karpov, J. Zmuidzinas, T. Phillips, N. Erickson, J. Swift, Y.-H. Chung,R. Lai, H. Wang; “THz Frequency Receiver Instrumentation for Herschel'sHeterodyne Instrument for Far Infrared (HIFI)”; Dec. 22, 2004,incorporated herein by reference.

Similarly, coupling of nanotubes to transistors and integration ofnanotubes with transistors have been described in the references, e.g.A. Javey, J. Guo, D. B. Farmer, W. Wang, E. Yenilmez, R. Gordon, M.Lundstrom, and H. Dai, “Self-Aligned Ballistic Molecular Transistors andElectrically Parallel Nanotube Arrays,” Nano Letters, vol. 4, p. 1319,2004; A. Javey, J. Guo, D. B. Farmer et al., “Carbon NanotubeField-Effect Transistors With Integrated Ohmic Contacts and High-k GateDielectrics,” Nano Letters, vol. 4, p. 447, 2004; J. Guo, J. Wang, E.Polizzi, Supriyo Datta and M. Lundstrom and H. Dai, “Electrostatics ofNanowire Transistors,” IEEE Transactions on Nanotechnology, vol. 2, p.329, December 2003; and A. Javey, J. Guo, Q. Wang, M. Lundstrom and H.Dai, “Ballistic Carbon Nanotube Field-Effect Transistors,” Nature, vol.424, p. 654, 2003 each of which is incorporated herein by reference.

Returning to the description of exemplary transistor 908, upon arrivalof an optical wave at the optical antenna element, the inducedelectrical signal in the optical antenna element 102 produces a changein a field in the gate 912 of the transistor that produces acorresponding amplified output according to principles of transistoroperation. The transistor may be configured for additional gain,selectivity, or interaction with the electronic circuitry. For example,the channel width and other parameters may be configured to be resonantat a frequency corresponding to the frequency of an input wave. Anexample of transistors configured for resonant operation is described inV. Ryzhii, I. Khmyrova, M. Shur; “Terahertz photomixing in quantum wellstructures using resonant excitation of plasma oscillations”; Journal ofApplied Physics; Feb. 15, 2002; pp. 1875-1881; Volume 91, Number 4;American Institute of Physics and in W. Knap, Y. Deng, S. Rumyantsev, M.S. Shur; “Resonant detection of subterahertz and terahertz radiation byplasma waves in submicron field-effect transistors”; Applied PhysicsLetters; Dec. 9, 2002; pp. 4637-4639; Volume 81, Number 24; AmericanInstitute of Physics.

It is noted that the components of the traditional diode (see FIG. 8) ora Schottky diode 1003 (FIG. 10), or the transistor that is associatedwith the optical antenna element 102 (see FIG. 9) can either be formedeither on, or in, the substrate 202 as shown in FIGS. 3, 4, 5 a, and 5b. As device speeds increase due to improvements in technology, theparticular device that is selected to be associated with the opticalantenna assembly may vary depending upon the application, configuration,frequency, fabrication considerations, or other considerations. As such,in this disclosure, the particular processing or mixing devicesdescribed herein are illustrative in nature, and not limiting in scope.

Moreover, many embodiments of the optical antenna elements 102 asdescribed relative to FIGS. 8 and 1 through 5 b can be formed partiallyor entirely with metal, semiconductors, carbon, or other materials thatmay be compatible with fabrication processes for many types ofelectronic components. Consequently, portions of the optical antennaelements 102 can correspond to or be integral with the portions of oneor more Schottky diodes, transistors, or other components. For example,where an optical antenna element 102 is metal, it may be integral withor actually form an electrode of the Schottky diode 1003 as shown inFIG. 10.

In a number of embodiments, signal processing techniques may be used toprocess and/or transfer information derived from one optical antennaassembly to another location. One signal processing technique that isparticularly applicable is conversion between the time domain and thefrequency domain. For example, the detected intensity values for areceiving optical antenna assembly can be sampled, and the quantizedsampled values converted, such as with a Fourier Transform orFast-Fourier Transform filter to obtain frequency domain informationthat is representative of the light received at all of the opticalantenna elements across the receiving optical antenna assembly. Thisfrequency domain information can be processed, stored, or transferred toa different location depending upon the desired use of the receivingoptical antenna assembly.

An inverse operation can generate a desired light signal or image withthe transmitting optical antenna assembly applies frequency domaininformation to such a device, such that the device selectively emits theequivalent of a spatial Fourier transform of an intended image. As isknown, a conventional lens can act as a spatial Fourier transformingdevice and thus can convert the waves emitted by the optical antennaassembly to a “real world” image represented by the information appliedto the optical antenna assembly.

In one embodiment, the optical antenna controller 1700 as described withrespect to FIG. 19 may generate the spatial frequency domain informationto be applied to the optical antenna assembly, from conversion of a realworld image, from an analytical source, such as optical design,modeling, or analysis software, or from information supplied fromanother source.

Examples of Oscillators

In many embodiments of the generating optical antenna assemblies thatgenerate light as described with respect to FIG. 2, electrical circuitrymay generate a carrier signal (either an electrical or optical signal)that is used to produce the light. Many embodiments of an oscillator maybe used to produce a sinusoidal carrier signal and/or reference signal.Examples of oscillators operating at, or near optical frequencies can befound in J. C. Pearson, I. Mehdi, E. Schlecht, F. Maiwald, A. Maestrini,J. Gill, S. Martin, D. Pukala, J. Ward, J. Kawamura, W. R. McGrath, W.A. Hatch, D. Harding, H. G. LeDuc, J. A. Stern, B. Bumble, L. Samoska,T. Gaier, R. Ferber, D. Miller, A. Karpov, J. Zmuidzinas, T. Phillips,N. Erickson, J. Swift, Y.-H. Chung, R. Lai, and H. Wang, ProceedingsSPIE, Astronomical Telescopes and Instrumentation, Waikoloa, Hi., 22-28Aug. 2002; John Ward, Frank Maiwald, Goutam Chattopadhyay, ErichSchlecht, Alain Maestrini, John Gill, and Imran Mehdi, 1400-1900 GHzLocal Oscillators for the Herschel Space Observatory, Proceedings,Fourteenth International Symposium on Space Terahertz Technology, pp.94-101, Tucson, Ariz., 2003; John Ward, Goutam Chattopadhyay, AlainMaestrini, Erich Schlecht, John Gill, Hamid Javadi, David Pukala, FrankMaiwald, and Imran Mehdi, “Tunable All-Solid-State Local Oscillators to1900 GHz,” Proceedings, Fifteenth International Symposium on SpaceTerahertz Technology, Amherst, Mass., 2004, each of which isincorporated herein by reference.

FIG. 11 shows one generalized representation of a feedback system thatmay operate as an oscillator 1102. Such basic diagrammatic structuresare commonly described in a variety of technologies, such as thoserelating to control systems, antenna systems, microwave systems, andanalog circuits. Generally speaking an input signal arrives at thesummer Σ where it is combined with a feedback signal from a feedbackelement f₁ to produce an combined signal that drives a gain element G.The gain element G amplifies the combined signal to produce an outputsignal V_(OUT).

Where the loop gain is greater than unity, the system output signal willgrow until some other system parameter limits the overall loop gain.Where the system is intended as an oscillator, the feedback element f,may be a frequency filter so that the overall system oscillations aresinusoidal at a selected frequency.

While one basic form of the oscillator 1102 is presenteddiagrammatically in FIG. 11, one skilled in the art will recognize thatthe actual oscillator configuration will depend upon the particularapplication, including frequency of operation, type of gain element,desired or available quality factor Q of various components and filters,and other operational and design considerations. For example, thefrequency may be determined in part or in whole by a frequency selectivecomponent of the gain element G. Thus, references to the feedbackelement f₁ herein may be applicable to the forward gain portion of thesystem, in lieu of, or in addition to the feedback portion of thesystem.

Moreover, systems involving more than one feedback loop, systems havinga separate driving source for gain, and systems having the gain andfeedback portions integral to a single component may be appropriate forcertain applications. Additionally, oscillators or signal sources may bepresented in a variety of other diagrammatic or conceptualrepresentational approaches.

In a general case, the oscillator output signal V_(OUT) can drive one ormore antenna elements described elsewhere herein. Where the outputsignal V_(OUT) is at optical frequencies, it may provide a carriersignal, driving signal, or reference signal directly, or may befrequency converted to produce a carrier signal, reference signal, ordriving signal for the optical antenna element.

While the feedback element f₁ is represented as a basic diagrammaticblock in FIG. 11, FIG. 12 shows, representationally, one type ofstructure 1202 that can, in part, define the system frequency ofoscillation and Q. In this system, a molecule or other structure, suchas a quantum dot, which may be a separate element or may be incorporatedinto a larger structure, such as a crystal lattice, receives inputenergy. The received energy may come in part from the system output,V_(out) as shown in FIG. 12. The structure 1202 resonates at a frequencydefined, in part, by its physical and electromagnetic characteristics,such as available quantum states of electrons or mass of molecules. Oneskilled in the art will recognize that FIG. 12 is merelyrepresentational of molecular structures where a nucleus N is surroundedby electrons e-. The energy levels, bond strengths, and other aspects ofthe molecular structure define resonances at which the molecule willnaturally respond, and FIG. 12 is presented representationally forclarity of presentation. Moreover, oscillators need not rely on naturalfrequencies of molecules in many applications. For example, oscillatorsemploying molecular or quantum dot based resonators have been producedat a variety of frequencies. For example, lasing based upon quantum dotoscillations is described in “Lasing from InGaAs/GaAs quantum dots withextended wavelength and well-defined harmonic-oscillator energy levels,”G. Park, O. B. Shchekin, D. L. Huffaker, and D. G. Deppe, AppliedPhysics Letters Vol 73(23) pp. 3351-3353. Dec. 7, 1998.

In some implementations, the feedback element f₁ may include a pluralityof separate or integral structures, components, or elements that providefeedback and/or frequency selectivity. As noted previously, suchstructures may be in the feedback portion of the system, in the forwardgain portion of the system, or in both.

While the description of FIG. 11 presents the oscillator, other sourcesof a carrier signal, reference signal, or driving signal may beappropriate in many cases. For example, one embodiment of a system thatmixes the reference signal with a received signal employs a separatelygenerated reference signal at the optical frequency. In one approach, alaser, such as a microlaser, laser diode, dye laser, or other type ofknown laser produces the reference signal.

In such systems, the output signal is typically an optical beam, at afrequency on the order of tens to hundreds of terahertz. The type oflasers selected may depend upon the desired wavelength, power, cost,portability or other aspects.

In one configuration, the signal from the reference source is directedtoward one or more of the optical antenna elements 102. As describedpreviously, the optical antenna elements convert energy in the incidentreference beam into a reference electrical signal carried by a portionof the optical antenna element 102.

The signal from the reference source may be applied to the same opticalelement that is operating as a receiving optical antenna element toproduce a response in the optical antenna element 102 that is acomposite of the response corresponding to the received optical signaland the response corresponding to the reference optical signal. Anexample of a reference optical signal mixed with a second signal todrive a dipole antenna is described in the article I. C. Mayorga, M.Mikulics; M. Marso; P. Kordos; A. Malcoci; A. Stoer; D. Jaeger; R.Gusten; “THz Photonic Local Oscillators”; September 2003;Max-Planck-Institute for Radioastronomy, which is incorporated herein byreference, and as obtained from the site:http://damir.iem.csic.es/workshop/files/03092003_(—)17h50_Camara.pdf.

Alternatively, as shown in FIG. 13, the signal from a reference source1302 may be applied to optical antenna elements 102A different from theoptical antenna elements 102 operating as receiving optical antennaelements. The electrical signal corresponding to the received opticalsignal, and the electrical signal corresponding to the reference opticalsignal, can then both be coupled to an electrical conductor 1304, suchas a waveguide, component, or polariton propagating material, thatproduces an output that is a composite of the electrical signal. Such anapproach may be applicable in a variety of other physicalconfigurations, and may be complementary to the approaches describedbelow with reference to FIGS. 15 and 16.

In another alternative approach, a reference signal may be formedaccording to optical irradiation of semiconductor or nonlinear opticalmaterials that, in turn, produce polariton propagation as can be foundin N. Stoyanov, D. Ward, T. Feurer, K. Nelson; “Terahertz polaritonpropagation in patterned materials”; Nature Materials-Letters; October2002; pp. 95-98; Volume 1; Nature Publishing Group, which isincorporated herein by reference. In such an approach, generatedpolaritons arriving at an optical antenna element or at an electroniccomponent provide a phase reference for electrical signals produced bythe optical antenna element.

Examples of Phase Comparators

FIG. 14 shows diagrammatically one embodiment of a phase comparator 1400that includes a combined optical antenna element array 1402 and areference waveform generator 1404 that produces a reference waveform1407, presented as traveling left to right in FIG. 14. One skilled inthe art will recognize that the diagrammatically represented componentsmay form a portion of an optical antenna assembly, as describedhereinabove. Each optical antenna element 102 in the array may generateand/or receive any given phase with respect to the other optical antennaelement in any desired spatial location. Control of the relative phasesbetween the optical antenna elements can allow beamforming, gaincontrol, or other features, as described previously.

In a receiving configuration, as illustrated in FIG. 14, the combinedoptical antenna element array 1402 includes a number of receivingoptical antenna elements 102 and corresponding comparators C_(X) (whereX=1, 2, 3, . . . , n). Each comparator C_(X) also receives the referencewaveform 1407 at a respective relative phase. In the receivingconfiguration, the comparator C_(X) compares the phase of the signalreceived by the optical antenna element 102 relative to the referencewaveform 1407 to determine the relative phase of the receive signals ateach optical antenna element 102.

Where the direction of field of interest is to be controlled, thecomparators C_(X) may include respective phase adjusters Δ φ_(X), thatshift the phases of the corresponding signals received by theirrespective optical antenna elements. One skilled in the art willrecognize that the same basic structure may be applied to a transmittingor generating embodiment, where combiners would be incorporated insteadof the comparators. Moreover, the representation of FIG. 14 isdiagrammatic and some of the aspects presented separately or as integralin FIG. 14 may be realized in one or more components in someconfigurations. For example, the phase comparator may be integral to theoptical antenna elements or combiners in some configurations and thephase adjusters may be integrated into a single component or a fewcomponents that may be separate from the combiners. Moreover, thecomparators or phase adjusters may be active or passive structures.

Additionally, the relative positions and/or orientations of the devicesor components may be changed or even reversed depending upon theselected system architecture. For example, the phase adjusters may bepositioned to control the phase of the reference signal in a receivingconfiguration or may be positioned to adjust the phase of the generatedsignals after the signals can be emitted by their respective opticalantenna elements.

With the embodiment of the reference planar waveform generator 1404 asdescribed with respect to FIG. 14, the reference waveform arrives from adirection substantially parallel to a plane containing the array of theoptical antenna elements (e.g., from left to right in FIG. 14) such thateach of the optical antenna elements receives the reference planarwaveform at a respective relative time. In such configurations where thereference waveform travels in, or at an angle non-orthogonal to, a planecontaining or parallel to the optical antenna elements as represented inFIG. 14, the relative time difference will be, at least in part, afunction of the inter-element spacing and the propagation velocity ofthe reference waveform.

In the configuration of FIG. 15, the reference wave arrives at all ofthe optical antenna elements or combiners 1502 substantiallysimultaneously. Here, the reference waveform is presented as travelingparallel to the central direction of the generated or received waveform,though other orientations may be selected depending upon designconsiderations. The applied reference waveform therefore moves in agenerally upward direction as illustrated with respect to FIG. 15. Inthis representation, the reference waveform thus arrives orthogonallyrelative to the plane containing the optical antenna elements. Anglesother than parallel or orthogonal to the plane containing the opticalantenna elements may also be selected. One approach to providing thereference waveform was described above with reference to FIG. 13,although the reference waveform may be a signal carried along aconductor, such as a wave of polaritons having defined relative phases.Such waves have been presented and imaged in the literature, e.g., DavidW. Ward, Eric Statz, Jaime D. Beers, Nikolay Stoyanov, Thomas Feurer,Ryan M. Roth, Richard M. Osgood, and Keith A. Nelson, “Phonon-PolaritonPropagation, Guidance, and Control in Bulk and Patterned Thin FilmFerroelectric Crystals,” in Ferroelectric Thin Films XII: MRS SymposiumProceedings, Vol. 797, edited by A. Kingon, S. Hoffmann-Eifert, I. P.Koutsaroff, H. Funakubo, and V. Joshi (Materials Research Society,Pittsburgh, Pa., 2003), pp. W5.9.1-6.

Also, although the reference above has been to a plane containing theoptical antenna elements, other non-planar structures, including curved,layered, or other configurations may be selected. In each of theseconfigurations, one or more reference signals may be supplied to theoptical antenna elements. Further, although FIG. 14 presents thereference signal as arriving from a direction perpendicular to a planecontaining the optical antenna elements and FIG. 15 shows the referencesignal as arriving from “behind” the optical antenna elements, in someapproaches the reference signal may arrive from the “front” of theoptical antenna elements. That is, the reference signal and thegenerated or received signal may arrive or depart from the same generalside of the optical antenna assembly. Moreover, other embodiments mayemploy more than one reference signal and may employ combinations ofreference signals.

Additionally, the reference waveform need not be a planar waveform, oreven a substantially planar waveform. For example, non-planar waveformsmay be desirable in some applications. One relatively straightforwardapproach to producing a non-planar reference waveform is to insert anon-uniform phase delay structure, such as a non-uniform phase plate oran active array of phase delay structures between the reference waveformgenerator 1404. Where the optical antenna element array 1402 isconfigured as an optical receiver, signals from the reference planarwaveform generator 1404 received at different times (and as such,signals received in different phases) among the different opticalantenna elements, may be monitored and adjusted, or otherwiseconsidered. As an example, assume that the phase of a signal generatedor received at a first optical antenna element 102 relative to thereference signal differs from the phase of a signal a second opticalantenna element 102.

Where the reference waveform is formed from polaritons, the referencewaveform may be a composite formed from a set of polariton generators,such as a set of emissive structures or a set of apertures in amaterial.

In one embodiment, the phase adjusters Δ φ_(R) can be controlled by anelectronic controller to include, e.g., a general-purpose computer, amicrocontroller, a microprocessor, an application-specific integratedcircuit, or any other type of computer-based, logic-based, mechanicalcontroller, electro-mechanical controller, or other type of acontroller. The controller can optionally have input from the user tocontrol the beamforming, beam steering, or other operations. Phaseadjusting of signals may be accomplished according to a variety of knowntechniques that may be adapted to the frequencies herein. In astraightforward case, a fixed phase mask may be defined to provide apassive form of phase control. One such approach to phase control isdescribed in “Coherent optical control over collective vibrationstraveling at light-like speeds,” R. M. Koehl and K. A. Nelson, J. Chem.Phys. 114, 1443-1446 (2001); “Spatiotemporal coherent control of latticevibrational waves,” T. Feurer, J. C. Vaughan, and K. A. Nelson, Science,299 374-377 (2003); and “Typesetting of terahertz waveforms,” T. Feurer,J. C. Vaughan, T. Hornung, and K. A. Nelson, Opt. Lett. 29, 1802-1804(2004), each of which is incorporated herein by reference.

In such a circumstance, the phase adjusters Δ φ_(R) of at least one ofthe two optical antenna elements 102 can be adjusted to reduce,eliminate, or otherwise control the in relative phases. The amount,direction, and other aspect of the relative phases can be determinedaccording to the desired response of the antenna assembly 100. Forexample, pairs of elements may be excited and the relative minima andmaxima of their farfield patterns may be determined. Alternatively, thegeneral gain of the optical antenna elements along paths may bemonitored and the relative phases of one, two, or more of the opticalantenna elements adjusted according to an intelligent searching approachto establish the beam pattern according to a determined set of criteria(e.g., side lobe levels, central lobe gain, or similar criteria.).

FIG. 16 shows another embodiment of phase comparator 1600 that compares,and adjusts, the phase of a reference signal that is generated bymultiple receiving optical antenna elements (instead of a referencesignal being received as in the embodiment of FIGS. 14 and 15). Therelative phases of the relative optical antenna elements 102 can beadjusted by adjusting the respective phase adjusters Δ φ_(T). The phasecomparator 1600 of FIG. 16 differs from the phase comparator 1400 ofFIG. 14 in that the reference planar waveform generator 1604 isconfigured to apply a reference wave that is perpendicular to theorientation of the optical antenna elements of the combined generatingvisible frequency element array 1602. As such, the reference waves canbe received at each of the multiple receiving optical antenna elements102 at a different time corresponding to the time necessary for thereference wave to travel to each respective optical antenna element froma preceding optical antenna element.

Examples of Regular Configurations of Optical Antenna Elements

Optical antenna elements may be fabricated according to a variety oftechniques including, but are not limited to, photolithography,lithography, nano structure growth, and attaching separately grown nanostructures a substrate or other support. Optical antenna elements may beclassified as either regular or non-regular. As described above, with anthis disclosure, the term “uniform”, pertains to regular orstatistically regular arrays of optical antenna elements that extendsubstantially continuously across a portion of, or an entirety of, anoptical antenna assembly.

Conceptually, perhaps one easy configuration of optical antenna elementsto consider are those in which each optical antenna elements areuniformly spaced from the neighboring optical antenna element, and eachoptical antenna element extends substantially perpendicular to thesubstrate or other supporting member. As the dimensions of each opticalantenna element are typically minute spacing of the optical antennaelements may not be exactly regular. Additionally, it might be difficultin many embodiments to ensure that the optical antenna elements extendsubstantially perpendicular to the substrate or supporting member. Assuch, the term “regular” pertains in many embodiments to the location ofattachment of the optical antenna elements across the substrate. Forexample, growing optical antenna elements from a number of regularlyspaced seed locations can produce a substantially regular array ofoptical antenna elements within an optical antenna assembly, even thoughmany of the optical antenna elements may extend at angles other thanorthogonal with respect to the substrate, as represented in FIG. 22. Fora large number of the optical antenna elements and a limited range orappropriate distribution of angles at which the optical antenna elementsextend from the supporting structure, the overall resulting operatingcharacteristics of many embodiments of the optical antenna assembly mayhave substantially repeatable, predictable and/or determinableelectromagnetic characteristics.

A large number of other fabrication techniques can be used to produceregular arrays of optical antenna elements. For example, lithographicpatterning techniques, e-beam lithography, and nano structure epitaxialgrowth can be utilized. Grown nanostructures can be separated, andreattached to the supporting member to produce a statistically regularconfiguration of the optical antenna elements.

Another embodiment of regular optical antenna assembly is represented inFIG. 23, in which a number of patterned rectangles 2304 are formed in asubstantially horizontal configuration across the substrate orsupporting member. The patterned rectangles 2304 may be formed in oneembodiment using lithography, photolithography, or some other etching,growth or other fabrication technique.

The spacing and dimensions of the patterned rectangles is selected tocorrespond to the intended operational frequency of the optical antennaelements. Typical photoconductor or processing techniques can be used toproduce the structures, as are generally known by those skilled in theart of semiconductor processing.

Although the embodiment of FIG. 23 includes rectangular optical antennaelements 2304, a variety of other structures, including those havinghexagonal, circular, elliptical, or other cross-sections may beappropriate for some configurations. Moreover, although the opticalantenna elements 2304 are represented as structures that extend from abase, other structures, such as recesses, apertures, or voids orstructures that extend laterally or in other directions may be suitable.

Examples of Applications in Systems

This disclosure now provides a number of different embodiments of aplurality of optical antenna elements 102 that can be configured in anarray. A number of embodiments of optical antenna assemblies may beoperable to produce waves appropriate for interferometric applications.

Interferometric applications, including interferometer-based opticalimaging or measurement, include telescopes, including those that haveallowed astronomers to measure the diameter of stars, distancemeasuring, photolithographic applications, surface topology, speedmeasurement, surface topology measurements, distance measurements, and avariety of other applications. The configurations of suchinterferometers can apply similar principles to those described withrespect to FIGS. 6 and 7.

In addition to general measurement applications, coherent techniques canbe configured to provide a variety of embodiments of a holographicprojector, as described below, including holographic devices for imagepresentation. One embodiment of optical interferometers described withrespect to this disclosure includes solid state interferometers. Suchsolid-state optical-domain interferometers operate by mixing thereceived light, and extracting phase information from the mixed signalwithout leaving the optical domain. One aspect of certain embodiments ofthe optical interferometers can be characterized as operating as“digital interferometers.” In one approach a digital opticalinterferometers includes a digital computation device that selectivelycontrols the amplitude and/or phase of a number of the optical antennaelements. The selected relative phase and/or amplitude may be determinedanalytically, through calculations or other approaches, may bedetermined empirically, or may be retrieved from memory. In oneembodiment, solid state optical-domain interferometers can bemicroelectromechanical system (MEMS) based. In another embodiment, suchsolid state optical-domain interferometers can be configured to operaterelying upon non-MEMS optical switching techniques.

A variety of approaches to preparing or producing data to store inmemory or to provide to the computation device may be appropriate. Inone application, the data is generated by capturing an image, includingphase information with an optical antenna assembly-based device or othertype of holographic device.

A variety of numerical techniques, such as those known for conventionalphased arrays and holographic techniques, may be applied to produce thedigital data for captured, displayed, or projected images. In oneapproach where each optical antenna element produces a signal indicativeof an arriving wave, the input is sampled, typically at a frequencyapproaching, substantially equaling, or exceeding the frequency of thereceived light, and the sampled data is processed digitally. Computertechniques and hardware continue to increase processing speeds tofurther improve the accuracy and performance of the digital imaging.

In some applications, the data or information may be captured at a firstlocation, or set of locations, and then propagated to a second locationwhere an image is presented, as a display or holographically presentedimage. Moreover, the data or information to be generated may becompressed or replaced or supplemented by representative data toincrease the speed or reduce system burden for information transmission.

The number, arrangement, location, material, and other properties of theoptical antenna elements may vary greatly depending upon the particulardesign considerations. However, as an exemplary embodiment of anapplication that may utilize coherent imaging or interferometricapproaches, a receiving optical antenna assembly may operate similarlyto a miniaturized so-called Keck telescope or a very large array (VLA)radio telescope employing waves at optical frequencies.

Certain techniques described herein, relating to interferometers, canalso be applied to design and construct cameras that can be configuredas detectors, as described above. The basic interferometer approachcould therefore be applied to detectors formed from a regular ornon-regular array of optical antenna elements or sets of arrays ofoptical antenna elements. Depending upon various design considerations,the dimensions of the array may range from postage stamp size tobillboard size, and even outside of these dimensions. At some physicaloptical antenna element dimension, the optical antenna elements of theoptical antenna assembly can be fabricated to be self-supporting, and itmay be appropriate to fabricate the substrate separately from theoptical antenna elements. In other embodiments, the optical antennaelements can be supported separately from a substrate or set ofsubstrates.

One embodiment of the receiving optical antenna assembly can beconfigured to form one embodiment of an extremely “thin” imager. In suchan approach, the operational circuitry can be disposed in a separatestructure or may have integrated operational circuitry. In oneapplication, the imager may be configured as a portion of a camera thatmay allow the camera to have features different from conventionalcameras. In one approach, additional portions of the optical antennaassembly, such as a phase control assembly can provide directionality orgain that can supplement or replace some portion of the conventionalfocusing optics in a camera. In some applications, the imagerfunctionality may be sufficient to completely replace the conventionaloptics. In other applications, the imager functionality may incorporatea combination of conventional optics and an array of optical antennaelements.

Where the optical antenna assembly is used without separate discreteoptics or is configured with microoptics, the optical antenna-basedcamera can be configured with a thickness corresponding to the thicknessof a semiconductor-based chip integrated into the camera (e.g., havingdimension on the order of one or a few mm), and depending upon theapplication may have an acceptable effective aperture size, focal lengthor other properties.

In one embodiment, as described above, digital sampling provides aneffective Fourier Transform by controlling/activating selected elementsor phase controls. This may allow for a self-correlating optical imagingdevice. While above descriptions include periodically spaced arrays ofelements, other configurations may be selected. In one embodiment, oneor more optical antenna elements 102 form an annular ring on a substrate202 as presented diagrammatically below with respect to FIG. 17.

This configuration including phasel taps 1702 provides a discrete set ofphase directions that can adjust the relative phase. This can be viewedas a phase scanning version of pixels. The set of taps in effect definesthe “phasels” that mix light from various parts of the ring of opticalantenna elements. The number and spacing of the phasels determine theangular resolution, in part.

One such embodiment of electrical domain interferometer can beimplemented using certain digital approaches. For example in one aspect,phasel taps can be configured as the φ-adjusts that rely upon delaylines whose delay time can be individually modified. Another approach tophase control involves physically modifying the relative positions ordimensions of the optical antenna elements 102.

Yet another aspect of the φ-adjusts 104 includes approaches that controlrelative signal delays with something other than physical length (e.g.,altering material properties, constructing waveguides with reducedpropagation velocities, etc.). An example of such analysis in themicrowave range that would be substantially directly applicable to theoptical antenna assembly is described in Chiang, et al., Microwave PhaseConjugation Using Antenna Arrays, IEEE Transactions on Microwave Theoryand Techniques, Vol. 46, No. 11 (November 1998), which gives examples ofanalyses of 8-element and 40-element microwave antenna arrays, and whichis incorporated herein by reference. While such design or control may beperformed analytically, empirical or statistical approaches may also beapplicable. For example, statistical approaches to beam forming ordirectional determination may be applied to the optical antennaassembly.

Another embodiment of an optical antenna assembly-based device employsscanning techniques. In one embodiment, an image is displayed orcaptured by scanning and controlling a pixel by pixel basis. Scanningmay be by a physical device, such as a MEMS, acoustooptic, or similarscanner, may be implemented by controlling phase and amplitude of thesignals at each respective optical antenna element, or may be acombination of both.

Many signal switching or modulation techniques can provide selectivityof signals from respective ones or groups of optical antenna elements.For example, one exemplary approach applies interference of signals,with a structure such as a Mach-Zender interferometer to selectivelytransmit some or all of the signal from respective optical antennaelements to the respective desired locations.

In a simplistic example of interference according to the structure ofFIG. 13, energy is traveling, for example, from the left optical antennaelement 102A (left to right) mixes with a signal from the right opticalantenna element 102. If the signals have the same amplitude and are ahalf wavelength out of phase at a given location, to a first order, thenet signal at the location will be substantially zero. The amplitudewill vary depending upon the amplitude of the received signal relativeto the amplitude of the reference signal, and/or the relative phases ofthe signals.

Rather than attempting to detect in all directions from a set opticalantenna elements positioned within one plane, it may be desired in someembodiments of the optical antenna assembly, to use a plurality ofantenna assemblies, each having a respective field of regard. Each ofthe antenna assemblies may have a fixed field of regard, or may bescannable. Moreover, the respective fields of regard may benon-overlapping or partially overlapping.

Where the fields of regard are separate, it may be advantageous to varythe relative phases within a smaller range as compared to the phaseranges corresponding to addressing a larger field of regard. Directingrespective optical antenna assemblies at respective orientations canallow an overall system to monitor a wide range of fields of view or toemit light over a relatively wide range. In some cases, the size of thearrays of optical antenna elements may allow a plurality of arrays to beassembled in a single unit or a few units. This may enable a compactsystem with a relatively large field of view.

Consider a 2D array of the phasel taps that can be configured, in theembodiment as described with respect to FIGS. 1 and 2, as the φ-adjust104. The combiner 106, as described with respect to FIG. 1, isconfigured to mix the input from any group of optical antenna elementshaving the desired combination of phase delays between a minimum valueand a maximum value.

One relatively simple approach to increasing the response speed of thephasel taps (e.g., the φ-adjust 104) includes providing each of thephasel taps with a set of discrete phase delays, each corresponding torespective a substantially fixed angular increment or relative phases.The relative phases between respective optical antenna elements 102 canbe adjusted by selectively coupling one or more of the discrete phasedelays.

After signals from a plurality of the receiving optical antenna elements102 are down-converted (e.g., by mixing), the output down-convertedsignal is then processed with appropriate electronic circuitry. In oneapproach, the electronic circuitry includes an analog-to-digital (A/D)converter that produces a digital signal representative of thedown-converted signal. While the described implementation employselectronic circuitry including the A/D converter, a variety of otherapproaches to processing or otherwise handling downconverted signals maybe appropriate, including analog filtering, sampling, or other knownapproaches.

Examples of Configurations of Regular and Non-Regular Arrays of OpticalAntenna Elements

In many embodiments of the optical antenna assembly, an array of opticalantenna elements may be arranged in a pattern other than an N×N matrixwhere each location includes one or more antenna elements. One exampledescribed previously is the ring arrangement of FIG. 17.

In another arrangement, a set of antenna elements may be arrangedaccording to an N×N matrix of positions, with one or more of thepositions in the matrix being empty. In some cases, a substantialportion, which may be more than half of the positions, may be empty. Thepositioning, response, design and other features of such a design may bedetermined according to techniques for sparse-array antenna structures.Examples of such analyses may be found, for example, in AthleyOptimization of Element Position for Direction Finding with SparseArrays, self-identified as published at IEEE Proceedings of the 11^(th)Workshop on Statistical Signal Processing, Aug. 6-8, 2001 (Singapore).

A less than full (two-dimensional) array of optical antenna elements maysimplify fabrication and computation in some applications, whileproviding substantially the same information as a full array of opticalantenna elements. A more sparsely populated array may addresssubstantially the same field of view and acquire substantially the sameinformation by sequentially addressing a set of fields of view. In oneapproach such an array includes a set of associated φ-adjusts 104configured as phasel taps, or individually-controllable delay lines, asdescribed with respect to FIGS. 1 and 2. The output from the differentrelatively few sets of the optical antenna elements can be combined toproduce a set of information that approximates that of a more denselypopulated array.

A number of embodiments of the optical antenna assembly may includearrays of optical antenna elements that have periodic or aperiodicspacing of the optical antenna elements. Selection of periodic oraperiodic spacing, the inter-element spacings, or the selection ofpatterns may depend in part upon the shape, sidelobes, gain, complexity,or other design considerations. For example, in some approaches gain orantenna beam pattern may be directed toward high directionality to allowcommunication between two locations at relatively low power. This mayreduce the likelihood of third party detection or reduce powerconsumption in some applications.

For example, in one embodiment of the receiving optical antennaassembly, optical antenna elements may be formed directly atop asemiconductor wafer. In one approach, a portion of the electroniccircuitry or portions of the antenna assembly may be formed integral tothe semiconductor wafer.

In one embodiment, a plurality of optical antenna elements may be arearranged to form a pattern that is generally in the shape of an annularring, which may be generally circular or another shape. In oneembodiment, the annular ring generally follows the periphery of at leasta portion of the chip. In such a configuration some portion of thecontrol circuitry or other portions of the antenna assembly, such asphase adjusters, mixers, or combiners, that is associated with theantenna elements is partially or wholly surrounded by the annular ring.The effective diameter or other cross sectional dimension of the annularring thereby defines the effective aperture of the optical antennaelements.

Regularly shaped arrays are not limited to N×N squares or M×N or N×Nrectangular arrangements. Moreover, the arrangements are not limited tocircular rings, squares, or rectangles. A variety of arrangements may bedeveloped according to antenna design principles in a variety oftwo-dimensional or three dimensional configurations.

For example, certain embodiments of patterns of optical antennaassemblies include, but are not limited to, sets of optical antennaelements as arranged as an extended dipole, a sinusoidal shape, arepeatable curve, annular rings, or other mathematically or otherwiseanalytically definable arrays.

Other embodiments of optical antenna assembly configurations include,but are not limited to, non-repeatable curves, portions of the opticalantenna assembly formed on different layers, portions of the optical atthe assembly at different elevations (e.g., on a non-level layer),curved or U-shaped structures, discontinuous portions of optical antennaassemblies that form capacitive, inductive, or matching structures, etc.

Moreover, the optical antenna elements are not necessarily limited topositioning on a single level and patterns may subtend more than onelevel. For example, the optical antenna elements may be arranged ondifferent layers of substrate or may be distributed irregularly indepth.

As described previously, FIG. 17 shows one example of an array ofoptical antenna elements 102 arranged in non-regular pattern. The numberof optical antenna elements forming the ring may range from one pair toa large number (tens, hundreds, thousands, or more), depending uponvarious design considerations, such as power, resolution, cost, size,manufacturability, or other factors. The layouts of the optical antennaelements 102 as described with respect to FIGS. 17 to 19 may be intendedto be configured as either receiving or generating optical antennaelements or element that may both generate and receive, as describedwith respect to FIGS. 1 and 2.

The diameter of the ring approximates the effective aperture of eachoptical antenna assembly 100. Circuitry or other elements may be locatedadjacent to or integral with the respective optical antenna elements insome configurations. However, in the approach presented in FIG. 17,delay lines (phasel taps) 1702 link optical antenna elements to anoptical antenna controller 1700. In this embodiment, optical antennaelements that are oppositely positioned utilize respective pairs ofdelay lines 1702, though other arrangements may be selected. The delaylines may be fixed or may have variable delays. In one approach tovariable delay, as presented in this embodiment, each delay line has oneor more phasel taps (e.g., the φ-adjust 104 as described with respect toFIGS. 1 and 2) that can be switched on or off under control of thecentral circuitry or under other control.

The operation of the optical antenna assembly 100 is controlled by theoptical antenna controller 1700. In one embodiment, each opposed pair ofoptical antenna elements can be operated in tandem. The optical antennacontroller 1700 can operate using as many pairs of optical antennaelements 102 as are desired, from one pair to the number of pairs ofoptical antenna elements that can be present in the optical antennaassembly 100.

FIG. 18 illustrates another embodiment of the optical antenna assembly100 that includes another non-regular pattern of optical antennaelements 102 in two generally spiral-shaped patterns 1802, 1804. Eachoptical antenna element 102 in each spiral-shaped pattern has arespective distance from a geometric center of the pattern thatincreases as the distance along the spiral increases. As represented inFIG. 18, the distance to each optical antenna element generallyincreases as one follows each spiral-shape pattern 1802, 1804 in acounter-clockwise direction, though other spiral shapes and directionsmay be appropriate depending upon the configuration.

FIG. 19 illustrates yet another embodiment of the optical antennaassembly 100 that illustrates selectively using sets of antenna elementsto control effective antenna aperture or other characteristics. In thisexample, one pair of opposed optical antenna elements 102 can beconnected or operationally coupled by respective conductors 1902 and1904 to the optical antenna controller 1700. The spacing of this firstpair of opposed optical antenna elements 102 defines a first aperturespacing 1910. Another pair of opposed optical antenna elements 102 areconnected or operationally coupled by respective conductors 1906 and1908 to the optical antenna controller 1700. The spacing of the secondpair of opposed optical antenna elements 102 defines a second aperturespacing 1912. The embodiment of optical antenna assembly 100 asdescribed with respect to FIG. 19 can therefore utilize the firstaperture spacing 1910 and/or the second aperture spacing 1912.

While the number of optical antenna elements, or pairs of opposingoptical antenna elements, shown in the figures, is presented herein as aone or a few elements or pairs of elements, it is to be understood thatthe number and exact configuration of the optical antenna elementswithin any particular optical antenna assembly is a design choice, andvariations thereof are within the intended scope of the presentdisclosure. In addition, other regular patterns, non-regular patterns,or mixtures thereof of optical antenna elements to form an array arewithin the intended scope with present disclosure.

FIG. 20 shows one embodiment of the optical antenna controller 1700, asdescribed above with respect to FIGS. 17, 18, and 19. The opticalantenna controller 1700, whose components are shown in FIG. 3, comprisesa central processing unit (CPU) 2002, memory 2004, circuit portion 2006,and input output interface (I/O) 2008 that may include a bus (notshown). The optical antenna controller 1700 can be a general-purposecomputer, a microprocessor, a microcontroller, or any other knownsuitable type of computer, controller, or circuitry that can beimplemented on hardware, software, and/or firmware. The CPU 2002performs the processing and arithmetic operations for the opticalantenna controller 1700. The optical antenna controller 1700 controlsthe signal processing, computational, timing, and other processesassociated with generating or receiving light from the optical antennaassembly 100.

Certain embodiments of the memory 2004 include random access memory(RAM) and read only memory (ROM) that together store the computerprograms, operands, desired waveforms, patterns of opposed opticalantenna elements, operators, dimensional values, system operatingtemperatures and configurations, and other parameters that control theoptical antenna's operation. The bus provides for digital informationtransmissions between CPU 2002, circuit portion 2006, memory 2004, andI/O 2008. The bus also connects I/O 2008 to the portions of the opticalantenna assembly 100 that either receive digital information from, ortransmit digital information to, though one or more optical antennaelements 102.

I/O 2008 provides an interface to control the transmissions of digitalinformation between each of the components in the optical antennacontroller 1700. I/O 2008 also provides an interface between thecomponents of the optical antenna controller 1700 and different portionsof the optical antenna assembly 100. The circuit portion 2006 comprisesall of the other user interface devices (such as display and keyboard).In another embodiment, the optical antenna controller 1700 can beconstructed as a specific-purpose computer such as anapplication-specific integrated circuit (ASIC), a microprocessor, amicrocomputer, or the like.

In one embodiment, multiple layers of the optical antenna assembly arealso provided. The layers may be substantial copies of each other or mayhave differing configurations, spacing, properties, or other features.In another embodiment, the effective width of the annular ring of theoptical antenna elements can be adjusted by adjusting the number ofactive optical antenna elements that can be contained in each row, oralternatively by activating or deactivating certain ones of multipleannular rings of the optical antenna elements.

The optical antenna controller 1700, as described with respect to FIGS.17, 18, 19, and 20 can be configured to activate or deactivate certainones of the optical antenna elements. As such, the configuration andelement density of the array of optical antenna elements 102 within theoptical antenna assembly 100 can be controlled extremely quickly by someprogramming of the optical antenna controller 1700. Replication ofcertain ones of the optical antenna elements or redundancy may alsoprovide fault tolerance, compensate for physical imperfections, reduceeffects of contaminants, such as dust or dirt, add wavelengthselectivity, or provide other design freedoms.

Reflective, refractive, phase delay, diffractive and/or other opticaltechniques may be combined with the optical antenna assembly andapproaches described herein. For example, refractive lenses may bepositioned to provide a curvature to waves arriving at the array ofoptical antenna elements or a wavelength selective filter may reducelight at certain wavelengths to augment wavelength selectivity of theoptical antenna assembly.

In certain embodiments, it may be desired to provide a scratch-proofcoating above one, or an array of, the optical antenna elements toprotect and ensure the continued operation of the optical antennaelements. A coating of a suitable covering material such as artificialsapphire, silicon, or diamond can be deposited or otherwise positionedabove a any portion of, or substantially all of, the array of opticalantenna elements. In some applications, a coating, such as diamond, maybe provided over both sides while providing continued optical antennaelement operation. In certain embodiments, control circuitry or othercircuitry may be integral to or positioned in close proximity to theantenna assembly, and subsequently protected by such coating. Theconcepts of the coating can be sufficiently straight-forward andself-explanatory and are not displayed in any figure.

Examples of Applications

An optical system 250, shown diagrammatically in FIG. 21 includes both agenerating optical antenna assembly 100 a, which may be the same as thatdescribed with respect to FIG. 2, that provides illumination to anobject 252. Additionally, the embodiment may include a receiving opticalantenna assembly 100 b, such as that described with respect to FIG. 1,that can capture light that is reflected from the surface of theilluminated object 252. As represented diagrammatically in the opticalsystem 250, light generated from a generating optical antenna element102 a illuminates an object 252. A second optical antenna element 102 bthen captures a portion of light reflected from the object. One skilledin the art will recognize that the diagrammatic representation of FIG.21 is a simplified representation of illumination and capture light fromthe environment and that the light striking the object will typically bea function of light emitted from more than one optical antenna element.Similarly, in some applications, each optical antenna element 102 a, 102b may operate as both a signal generator and a signal receiver. Thesimplified representation is presented herein for clarity ofpresentation.

Where the generating optical antenna assembly 100 a is configured toconcentrate optical energy or direct optical energy toward one or moreregions, as described previously, the optical antenna assembly canselectively illuminate one or more spatial locations or angular ranges.Similarly, in one embodiment, the receiving optical antenna assembly 100b can receive light selectively from one or more regions or angularranges. In some approaches, a single optical antenna assembly may beconfigured to selectively direct optical energy to and receive opticalenergy from selected spatial locations or angular ranges.

In one embodiment, a combined illumination and reception technique usingthe optical antenna assemblies can be configured to operate similarly toan optical range finder or LIDAR type of system.

In some cases, the selectivity, gain, or other operational aspects maybe adjusted by selective polarization or by adding additional opticalstructures, such as diffractive elements, lenses, or other known opticalcomponents. While the above embodiment has been described in many casesas a coherent system, in some cases, an optical antenna assembly can beadapted to operate with non-coherent or only partially coherent lightenergy.

Often, illumination or illuminated imaging in the optical domain iseither broadband (e.g., a camera flash that outputs light to having awide mixture of light frequencies such as white light), or narrowband(i.e. light produced with a laser that has one, or a small number of,frequencies). In one embodiment, an optical antenna assembly can beconfigured to provide or receive light selectively from two, three, ormore wavelength bands. In one approach, the bands may be primary colorbands, such as red, green, and blue wavelengths. A multiband approach,such as light of the visible and/or near-visible frequencies, can alsobe used in various image capture or sensing applications. In each ofthese approaches, the antenna element sizes, spacings, orientations, andother characteristics can be optimized according to design criteria. Insome approaches, sets of antenna elements may be devoted to eachwavelength range.

While much of the above discussion of exemplary embodiments hasconcentrated on light of visible or infrared wavelengths, many of themethods, principles, structures, and processes herein may be applied ator extended to other wavelength bands. For example, wavelengths in thefar-infrared and into the millimeter wavelength range may penetratematerials to depths different from and, in some cases, greater thanvisible wavelengths. Such wavelength bands may be chosen for example toimage objects or augment imaging of objects. In one approach,wavelengths on the order of one or a few millimeters may permit imagingat depths different from those of visible wavelengths. Similarly, asphotolithographic techniques or other fabrication techniques permit,ultraviolet implementations may be realized.

CONCLUSION

While several embodiments of application for optical antenna elementshave been described in this disclosure, it is emphasized that theseapplications are not intended to be limiting in scope. Any device orapplication that involves the use of the optical antenna elements, asdescribed within this disclosure, is within the intended scope of thepresent disclosure.

Different embodiments of the optical antenna elements can be included insuch embodiments of the communication system as telecommunicationsystems, computer systems, audio systems, video systems,teleconferencing systems, and/or hybrid combinations of certain ones ofthese systems. The embodiments of the status indicator as described withrespect to this disclosure are intended to be illustrative in nature,and are not limiting its scope.

Those having skill in the art will recognize that the state of the arthas progressed to the point where, in many cases, there is littledistinction left between hardware, firmware, and softwareimplementations of aspects of systems; the use of hardware, firmware, orsoftware is generally (but not always, in that in certain contexts thechoice between hardware and software can become significant) a designchoice representing cost vs. efficiency tradeoffs. Those having skill inthe art will appreciate that there are various vehicles by whichprocesses and/or systems and/or other technologies described herein canbe effected (e.g., hardware, software, and/or firmware), and that thepreferred vehicle will vary with the context in which the processesand/or systems and/or other technologies are deployed. For example, ifan implementer determines that speed and accuracy are paramount, theimplementer may opt for a mainly hardware and/or firmware vehicle;alternatively, if flexibility is paramount, the implementer may opt fora mainly software implementation; or, yet again alternatively, theimplementer may opt for some combination of hardware, software, and/orfirmware. Hence, there are several possible vehicles by which theprocesses and/or devices and/or other technologies described herein maybe effected, none of which is inherently superior to the other in thatany vehicle to be utilized is a choice dependent upon the context inwhich the vehicle will be deployed and the specific concerns (e.g.,speed, flexibility, or predictability) of the implementer, any of whichmay vary.

The foregoing detailed description has set forth various embodiments ofthe devices and/or processes via the use of block diagrams, flowcharts,and/or examples. Insofar as such block diagrams, flowcharts, and/orexamples contain one or more functions and/or operations, it will beunderstood by those skilled within the art that each function and/oroperation within such block diagrams, flowcharts, or examples can beimplemented, individually and/or collectively, by a wide range ofhardware, software, firmware, or virtually any combination thereof. Inone embodiment, several portions of the subject matter described hereinmay be implemented via Application Specific Integrated Circuits (ASICs),Field Programmable Gate Arrays (FPGAs), digital signal processors(DSPs), or other integrated formats. However, those skilled in the artwill recognize that some aspects of the embodiments disclosed herein, inwhole or in part, can be equivalently implemented in standard integratedcircuits, as one or more computer programs running on one or morecomputers (e.g., as one or more programs running on one or more computersystems), as one or more programs running on one or more processors(e.g., as one or more programs running on one or more microprocessors),as firmware, or as virtually any combination thereof, and that designingthe circuitry and/or writing the code for the software and or firmwarewould be well within the skill of one of skill in the art in light ofthis disclosure. In addition, those skilled in the art will appreciatethat the mechanisms of the subject matter described herein are capableof being distributed as a program product in a variety of forms, andthat an illustrative embodiment of the subject matter described hereinapplies equally regardless of the particular type of signal bearingmedia used to actually carry out the distribution. Examples of a signalbearing media include, but are not limited to, the following: recordabletype media such as floppy disks, hard disk drives, CD ROMs, digitaltape, and computer memory; and transmission type media such as digitaland analog communication links using TDM or IP based communication links(e.g., packet links).

All of the above U.S. patents, U.S. patent application publications,U.S. patent applications, foreign patents, foreign patent applicationsand non-patent publications referred to in this specification and/orlisted in any Application Data Sheet, are incorporated herein byreference, in their entireties.

The herein described aspects depict different components containedwithin, or connected with, different other components. It is to beunderstood that such depicted architectures are merely exemplary, andthat in fact many other architectures can be implemented which achievethe same functionality. In a conceptual sense, any arrangement ofcomponents to achieve the same functionality is effectively “associated”such that the desired functionality is achieved. Hence, any twocomponents herein combined to achieve a particular functionality can beseen as “associated with” each other such that the desired functionalityis achieved, irrespective of architectures or intermedial components.Likewise, any two components so associated can also be viewed as being“operably connected”, or “operably coupled”, to each other to achievethe desired functionality, and any two components capable of being soassociated can also be viewed as being “operably couplable”, to eachother to achieve the desired functionality. Specific examples ofoperably couplable include but are not limited to physically mateableand/or physically interacting components structure and/or wirelesslyinteractable and/or wirelessly interacting components or structuresand/or logically interacting and/or logically interactable components orstructures and/or electromagnetically interactable and/orelectromagnetically interacting components or structures.

It is to be understood by those skilled in the art that, in general,that the terms used in the disclosure, including the drawings and theappended claims, are generally intended as “open” terms. For example,the term “including” should be interpreted as “including but not limitedto”; the term “having” should be interpreted as “having at least”; andthe term “includes” should be interpreted as “includes, but is notlimited to”; etc. In this disclosure and the appended claims, the terms“a”, “the”, and “at least one” are intended to apply inclusively to oneor a plurality of those items.

Furthermore, in those instances where a convention analogous to “atleast one of A, B, and C, etc.” is used, in general such a constructionis intended in the sense one having skill in the art would understandthe convention (e.g., “a system having at least one of A, B, and C”would include but not be limited to systems that have A alone, B alone,C alone, A and B together, A and C together, B and C together, and/or A,B, and C together, etc.). In those instances where a conventionanalogous to “at least one of A, B, or C, etc.” is used, in general sucha construction is intended in the sense one having skill in the artwould understand the convention (e.g., “a system having at least one ofA, B, or C” would include but not be limited to systems that have Aalone, B alone, C alone, A and B together, A and C together, B and Ctogether, and/or A, B, and C together, etc.).

Those skilled in the art will appreciate that the herein-describedspecific exemplary processes and/or devices and/or technologies arerepresentative of more general processes and/or devices and/ortechnologies taught elsewhere herein, such as in the claims filedherewith and/or elsewhere in the present application.

Within this disclosure, elements that perform similar functions in asimilar way in different embodiments may be provided with the same orsimilar numerical reference characters in the figures. The abovedisclosure, when taken in combination with the associated figures,represents a number of embodiments of arrays of optical antenna elementsincluded in optical antenna assemblies. Other slight modifications fromthese disclosed embodiments that are within the scope of the attachedclaims are also within the intended scope of the present invention.

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 86. An optical gain assemblycomprising: a. A first set of passive gain elements, each passive gainelement in the first set being sized and shaped to selective respond toa selected first optical frequency; and b. A second set of passive gainelements, each passive gain element in the second set being sized andshaped to selective respond to a selected second optical frequencydifferent from the first optical frequency.
 87. The optical gainassembly of claim 86 wherein each of the passive gain elements in thefirst set of gain elements includes at least one physical dimensioncorresponding to an integral number of quarter wavelengths of the firstoptical frequency.
 88. The optical gain assembly of claim 86 furthercomprising electrical circuitry having a first portion coupled to thefirst set of passive gain elements and being configured to respond tosignals at the first optical frequency or a harmonic of the firstoptical frequency.
 89. The optical gain assembly of claim 86 wherein theelectrical circuitry includes a second portion coupled to the second setof passive gain elements and being configured to respond to signals atthe second optical frequency or a harmonic of the second opticalfrequency.
 90. The optical gain assembly of claim 86 further comprisinga third set of passive gain elements, each passive gain element in thethird set being sized and shaped to selective respond to a selectedthird optical frequency different from the first optical frequency anddifferent from the second optical frequency.
 91. The optical gainassembly of claim 86 wherein the first and second sets of passive gainelements are substantially coplanar.
 92. The optical gain assembly ofclaim 91 further including a substrate carrying the first and secondsets of passive gain elements.
 93. A multifrequency optical antenna,comprising: a. A first set of antenna elements sized to respond to afirst optical frequency; b. A second set of antenna elements sized torespond to a second optical frequency; and c. A third set of antennaelements sized to respond to a third optical frequency, wherein thefirst, second and third optical frequencies are different opticalfrequencies.
 94. The multifrequency optical antenna of claim 93, furtherincluding a body carrying the first, second and third sets of antennaelements.
 95. The multifrequency optical antenna of claim 93, whereinthe first set of antenna elements is arranged spatially in a non-uniformpattern.
 96. The multifrequency optical antenna of claim 94 wherein thefirst and second sets of antenna elements are interleaved in asubstantially common plane.
 97. The multifrequency optical antenna ofclaim 93, wherein the first, second and third sets of antenna elementsdefine first, second and third planes respectively.
 98. Themultifrequency optical antenna of claim 93, further comprising first,second and third phase reference sources, wherein each of the first,second and third phase reference sources is coupled to each of thefirst, second and third sets of antenna elements respectively.
 99. Themultifrequency optical antenna of claim 93 wherein the antenna elementsin each of the first, second and third sets of antenna elements includesan output region, further including first, second and thirdelectromagnetic guiding structures coupled to the first, second, andthird sets of antenna elements respectively.
 100. A method of producingan electrical signal indicative of electromagnetic waves at at least twooptical frequencies, comprising: a. Selectively and passively extractingenergy from the electromagnetic waves at a first of the frequencies inthe at least two optical frequencies; b. Converting the selectively andpassively extracted energy at the first of the optical frequencies intoa form of energy guidable by electrons at the first optical frequency ora harmonic of the first optical frequency; c. Guiding the converted formof energy guidable by electrons at the first optical frequency or aharmonic of the first optical frequency to a first processing location;d. Processing the guided, converted form of energy guidable by electronsat the first optical frequency or a harmonic of the first opticalfrequency to a first signal indicative of the electromagnetic waves; e.Selectively and passively extracting energy from the electromagneticwaves at a second of the frequencies in the at least two opticalfrequencies; f. Converting the selectively and passively extractedenergy at the second of the optical frequencies into a form of energyguidable by electrons at the second optical frequency or a harmonic ofthe second optical frequency; g. Guiding the converted form of energyguidable by electrons at the second optical frequency or a harmonic ofthe second optical frequency to a second processing location; and h.Processing the guided, converted form of energy guidable by electrons atthe second optical frequency or a harmonic of the second opticalfrequency to a second signal indicative of the electromagnetic waves.101. The method of claim 100 further including processing the first andsecond signals indicative of the electromagnetic waves to produce acombined signal indicative of the electromagnetic waves.
 102. The methodof claim 100 wherein selectively and passively extracting energy fromthe electromagnetic waves at a first of the frequencies in the at leasttwo optical frequencies includes intercepting the energy from theelectromagnetic waves at a first of the frequencies in the at least twooptical frequencies with an antenna element having at least onedimension corresponding to an integral number of wavelengths of theextracted energy at the first frequency.
 103. The method of claim 100wherein processing the guided, converted form of energy guidable byelectrons at the first optical frequency or a harmonic of the firstoptical frequency to a first signal indicative of the electromagneticwaves includes mixing the guided, converted form of energy guidable byelectrons at the first optical frequency or a harmonic of the firstoptical frequency with a reference signal.
 104. The method of claim 103wherein processing the guided, converted form of energy guidable byelectrons at the first optical frequency or a harmonic of the firstoptical frequency to a first signal indicative of the electromagneticwaves further includes detecting a component of a signal produced by themixing.
 105. A method of producing electronically guided waves at aplurality of optical frequencies, comprising: a. Producing a firstvarying electrical potential along a first structure at a first opticalfrequency by interacting with an electromagnetic wave at the firstoptical frequency; b. Converting the first varying electrical potentialto a first guided wave; c. Producing a varying electrical potentialalong a second structure at a second optical frequency different fromthe first optical frequency by interacting with an electromagnetic waveat the second optical frequency; and d. Converting the second varyingelectrical potential to a first guided wave.
 106. The method of claim105 wherein producing the first varying electrical potential along thefirst structure includes orienting the first structure along an expectedarrival direction of the electromagnetic wave.
 107. The method of claim106 wherein converting the first varying electrical potential to a firstguided wave includes extracting energy from the varying electricalpotential at a selected location along the first structure.
 108. Themethod of claim 107 wherein extracting energy from the varyingelectrical potential at a selected location along the first structureincludes producing guided plasmons from the extracted energy.